NewSpace Market · Sector Catalogue
Structures & Mechanisms
Every unit we list in this sector — specifications, manufacturers and where to ask for a quote. Compiled from the live NewSpace Market catalogue.
About this catalogue
What is inside
This catalogue lists 323 structures & mechanisms products offered by 102 manufacturers across 25 countries. Of those, 124 carry a manufacturer datasheet and 21 publish a price; the rest are quoted on request — normal in this market, where configuration drives cost.
Entries are grouped alphabetically by manufacturer. Every product links back to its page on newspacemarket.com, where you will find the full specification, the datasheet and a quote form that reaches the manufacturer directly.
Compiled 15 October 2026 from the live catalogue. Specifications are as published by the manufacturers; we normalise units but do not re-measure. Where a figure looked implausible it was left out rather than guessed.
Manufacturers by country
Overview
All products at a glance
| Product | Manufacturer | Country | Key specification | Price |
|---|---|---|---|---|
| 104-pin Bus Reversing Adapter | Pumpkin, Inc. | United States | Connector: 104-pin CubeSat bus, stackthrough on one side, standard header o… | $110 |
| 10m-diameter flat-panel SAR antenna deployment mechanism | MinoSpace | China | Deployment drive: Passive spiral spring | on request |
| 12-Unit cubesat structure | ISISPACE Group | Netherlands | Manufacturer: ISISPACE | on request |
| 12U Structure | EnduroSat | Bulgaria | Dimensions: 226.3 x 226.3 x 454 mm | on request |
| 16-Unit cubesat structure | ISISPACE Group | Netherlands | Manufacturer: ISISPACE | on request |
| 16U satellite structure | GomSpace | Denmark | — | on request |
| 16U Structure | EnduroSat | Bulgaria | Dimensions: 226.3 x 226.3 x 366 mm | on request |
| 1P Skeleton Wall PocketQube Structure | Alba Orbital | United Kingdom | Dimensions: 1P (Unit) - 50 mm x 50 mm external dimensions. 47 mm x 47 mm in… | on request |
| 1U Cube Structure | Gran Systems | United States | Temperature: -50°C to +120°C | on request |
| 1U CubeSat Structure | CubeSat Aerospace | India | Dimensions: 100 mm × 100 mm × 113.5 mm | on request |
| 1U Cubesat Structure | Aphelion Orbitals | United States | Height: 113.5 mm | on request |
| 1U Quad CubeSat Boom Deployer | CTD (Composite Technology Development) | United States | Form factor: 1U CubeSat | on request |
| 2nd Switch (L2) Spring Upgrade Kit | Pumpkin, Inc. | United States | SKU: 711-01478 | $88 |
| 2P Skeleton Wall PocketQube Structure | Alba Orbital | United Kingdom | Dimensions: 2P (Unit) | on request |
| 3P Skeleton Wall PocketQube Structure | Alba Orbital | United Kingdom | Dimensions: 3P (Unit) | on request |
| 3POD | Comat | France | Pointing accuracy: 1° (worst case) | on request |
| 3U CubeSat Frame | Princeton Satellite Systems | United States | Mass: 0.350 kg | on request |
| 3U CubeSat Structure | Gran Systems | United States | Temperature: -50°C to +120°C | on request |
| 4500 Series Tee Type Filter Single Stage 3000 psi | VACCO Industries | United States | Operating pressure: 3000 PSIG | on request |
| 6U Cube Structure | Gran Systems | United States | Temperature: -50°C to +120°C | on request |
| A-Deck Adapter System | Adaptive Launch Solutions | United States | TRL: 8 | on request |
| Actuators and Servo Actuators | Moog Space Defense Group | United States | — | on request |
| ADACS Payload Walls / 1U Chassis MAI-100/MAI-200 Extension | Pumpkin, Inc. | United States | SKU: 703-00397 | $1 610 |
| APPMAX2 Electric Propulsion Pointing Mechanism | Beyond Gravity (ex-RUAG Space) | Switzerland | Axes: 2-axis pointing mechanism | on request |
| APPMAX3 Deployable Thruster Pointing Mechanism | Beyond Gravity (ex-RUAG Space) | Switzerland | Actuation: Three stepper motor-based actuators | on request |
| Asteria Adhesive Attachment Technology | Kall Morris Inc | United States | Adhesion type: Omnidirectional gecko adhesion | on request |
| Asteroid Refinery Technology | AstroForge | United States | Target metals: Platinum group metals (Pt, Pd, Ir, Rh, Os, Ru) | on request |
| Astrix Inflatable Deployment System | Astrix Astronautics | New Zealand | Deployment efficiency (space): 20x more space efficient | on request |
| Astrobrake | Gama Space | France | Mass: 900 g | on request |
| B-Flat | FAULHABER Drive Systems | Germany | — | on request |
| Beryllium Optical and Structural Components | materion | United States | Key material: Beryllium (density 1.85 g/cm³, modulus 287 GPa) | on request |
| Boom System | Frond Space Systems | New Zealand | Deployable length (initial): 2m | on request |
| Brushless DC-motors with integrated Speed Controller | BXT SC | FAULHABER Drive Systems | Germany | Speed range: [min-1] | on request |
| BryleeDrive Multi-Axis Micro-Drive | Micromotion GmbH | — | Motion type: Combined linear and rotary (multi-axis) | on request |
| Bundle (1p,1.5p,2p,2.5p) Skeleton Wall PocketQube Structures | Alba Orbital | United Kingdom | Dimensions: 1p,1.5p,2p,2.5p (Unit) | £9 999 |
| BX4 IMC | FAULHABER Drive Systems | Germany | — | on request |
| C14 Bi-Axis Gimbal | Sierra Space | United States | Actuator: C14 Incremental Rotary Actuator | on request |
| CADRE (Cooperative Autonomous Distributed Robotic Exploration) | Motiv Space Systems | United States | Client: NASA Jet Propulsion Laboratory | on request |
| Canadarm3 / Space Robotics Systems | MDA Space | Canada | Systems: Canadarm (Shuttle, retired), Canadarm2 (ISS), Canadarm3 (Lunar Gat… | on request |
| Carbon Fiber Composites for Space Structures | Toray Industries Space | Japan | Key products: T700SC/T800 carbon fibers, M-grade high-modulus fibers (M46J,… | on request |
| Ceramic Matrix Composite (CMC) Space Structures | MT Aerospace | Germany | — | on request |
| CFRP Engineering | Perigee Aerospace | South Korea | Diameter standard 1: 0.76 m | on request |
| COBRA-HPX Gimbal | Tethers Unlimited, Inc. (AMERGINT) | United States | Mass: 276 g | on request |
| COBRA™ Gimbal | Tethers Unlimited, Inc. (AMERGINT) | United States | Flight heritage: ! | on request |
| Cold Plates | Thermavant | United States | Materials: Al and Al composites (0 to T6 temper, most common); Cu and Cu co… | on request |
| Collapsible Tubular Mast (CTM) | Opterus Research and Development | United States | Diameter: 50-600 mm | on request |
| Common Space Vehicle Mechanisms | Northrop Grumman Space Systems | United States | Flight heritage: 40+ years, 100% mission success, over 50 missions | on request |
| Composite Radomes for Launchers and Satellites | Compoxi | Spain | — | on request |
| Composite Spacecraft Structures and Booms | CTD (Composite Technology Development) | United States | Products: Composite booms, solar array substrates, antenna reflectors, stru… | on request |
| Composite Structures and Assemblies | ACT (Advanced Cooling Technologies) | United States | Manufacturing process: 5-axis CNC machining, autoclave cure, aerospace-grad… | on request |
| Composite Technologies | DELTAV Space Technologies | Turkey | — | on request |
| Composites | Tata Advanced Systems (Space) | India | — | on request |
| Compoxi | Compoxi | Spain | — | on request |
| Compoxi Space Composite Manufacturing | Compoxi | Spain | Products delivered to orbit: 850 | on request |
| Compoxi Space Composite Structures & Components | Compoxi | Spain | — | on request |
| CSD-2A Component Set | Harmonic Drive | United States | Rated Torque L10: 3.7 Nm | on request |
| CSD-2UF Gear Unit | Harmonic Drive | United States | Rated Torque L10: 3.7 Nm | on request |
| CSD-2UH Gear Unit | Harmonic Drive | United States | Reduction ratios: 30:1 to 160:1 | on request |
| CSF-1U-CC Miniature Gear Units | Harmonic Drive | United States | Zero backlash: Yes | on request |
| CSF-1U-CC-F Miniature Gear Units | Harmonic Drive | United States | Zero backlash: Yes | on request |
| CSF-1U-F Miniature Gear Units | Harmonic Drive | United States | Outline Dimensions: 20 mm~51 mm | on request |
| CSF-2A | Harmonic Drive | United States | Rated Torque L10: 0.9 Nm | on request |
| CSF-2UH-LW Gear Unit | Harmonic Drive | United States | Zero Backlash: Yes | on request |
| CSF-2UP | Harmonic Drive | United States | — | on request |
| CSF-2UP Ultra Flat Gearhead | Harmonic Drive | United States | Ratios: 30:1 to 100:1 | on request |
| CSF-2XH Miniature Gear Units | Harmonic Drive | United States | Gear Ratios: 30:1 to 100:1 | on request |
| CSF-8-30-1U-CC-F Miniature Gear Units | Harmonic Drive | United States | Series: CSF | on request |
| CSF-GH Harmonic Drive® gearhead | Harmonic Drive | United States | Peak Torque: 18 Nm to 2,630 Nm | on request |
| CSG-2A Component Set | Harmonic Drive | United States | Peak Torque: 23 Nm to 3419 Nm | on request |
| CSG-2UH Zero Backlash Gear Unit | Harmonic Drive | United States | Peak Torque: 23 Nm to 3419 Nm | on request |
| CSG-2UH-LW Gear Unit | Harmonic Drive | United States | Peak Torque: 23 Nm to 3419 Nm | on request |
| CSG-GH | Harmonic Drive | United States | Peak Torque: 23 Nm to 3,419 Nm | on request |
| CTD Composite Deployable Structures | CTD (Composite Technology Development) | United States | Products: Deployable booms, solar array structures, antenna reflectors | on request |
| CubeSat Aerospace Satellite Structures (1U–6U) | CubeSat Aerospace | India | 1u dimensions: 100 × 100 × 113.5 mm | on request |
| CubeSat Kit Quad-switch Cover Plate Assembly | Pumpkin, Inc. | United States | Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) | $865 |
| CubeSat Kit™ Base Plate Assembly | Pumpkin, Inc. | United States | Configuration option: type: Solid-Wall, Skeletonized | $690 – $1 560 |
| CubeSat Kit™ Base Plate Assembly for AntS Antenna | Pumpkin, Inc. | United States | Configuration option: separation switch: Dual | $1 085 |
| CubeSat Kit™ Chassis Walls | Pumpkin, Inc. | United States | Configuration option: size: 0.5U, 1U, 1.5U, 2U, 3U | $1 215 – $2 955 |
| CubeSat Kit™ Cover Plate Assembly | Pumpkin, Inc. | United States | Configuration option: type: Solid-Wall, Skeletonized | $495 |
| CubeSat Kit™ Cover Plate Assembly for AntS antenna | Pumpkin, Inc. | United States | Configuration option: separation switch: None, Dual | $955 – $1 085 |
| CubeSat Kit™ Large Aperture Base Plate Assembly, Dual Switch | Pumpkin, Inc. | United States | SKU: 710-02203 | $820 |
| CubeSat Kit™ Large Aperture Cover Plate Assembly | Pumpkin, Inc. | United States | Configuration option: separation switch: None, Dual | $690 – $820 |
| CubeSat Kit™ Payload Adapter Plate | Pumpkin, Inc. | United States | Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) | $360 |
| CubeSat Kit™ Payload Cover Plate Assembly | Pumpkin, Inc. | United States | Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) | $495 |
| CubeSat Kit™ Pro Chassis Walls | Pumpkin, Inc. | United States | Configuration option: size: 0.5U, 1U, 1.5U, 2U, 3U | $22 500 – $39 500 |
| CubeSat Structural Frame | NanoAvionics | Lithuania | Material: 7075-T7351 aluminum alloy | €5 040 |
| CubeSat Structure (1U / 2U / 3U) | KSF Space Foundation | United States | Available sizes: 1U, 2U, 3U | $1 000 |
| CubeSat Structures (Boltless Structure) | Boltless CubeSat Structures (Kikuchiseiki, KIKUCHI SEIKI) | Japan | Structure type: Boltless Structure | on request |
| CubeSat Transporter | CubeSat Aerospace | India | Supported sizes: 1U, 1.5U, 2U, and 3U CubeSats (interchangeable inserts) | on request |
| Custom Mechanisms (Mastcam-Z, SOMS Filter Wheel, Mastcam-Z Filter Wheel) | Motiv Space Systems | United States | Mastcam-z key capabilities: High-Definition Video | on request |
| Custom PocketQube Structural Panel | Alba Orbital | United Kingdom | Dimensions: 1p/1.5p/2p/3p | on request |
| Custom SMA Actuators | Memetis | — | Actuator types: Linear, Spiral, Bending, Antagonistic Linear | on request |
| Damper | MinoSpace | China | — | on request |
| DDP Servo Drive | Harmonic Drive | United States | Supply Voltage (DDP-090-09): DC24V | on request |
| Deployable Space Structures | Prosix Engineering | Spain | Space deployable masts - length: 1 – 50 meters long | on request |
| Deployable Space Structures (General) | L.Garde Inc | — | Isat array length: 300 meters | on request |
| Deployable Tape Truss Boom | MMA Design | — | Expansion ratio: Up to 100:1 | on request |
| Deployment Mechanisms for Satellites (Solar Arrays, Antennas & Instruments) | Arquimea | Spain | Reference application: 1 × 1 m solar array release and deployment mechanism | on request |
| Detonators | PacSci EMC | United States | Design: Wide range of compact designs with extreme temperature capability | on request |
| Direct Drive and Hollow Shaft Motors | Harmonic Drive | United States | Positioning accuracy: 10 arc-sec | on request |
| Docking Plate | Astroscale US | Japan | Generation: Second generation (flight-proven) | on request |
| E-ELT – European Extremely Large Telescope | EIE Space Technologies Srl | Italy | Primary Mirror Diameter: 39 m | on request |
| EBAD NEA® Model 2545 Pin Puller | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Pull force at beginning of stroke: 45 lbf (200 N) | on request |
| EBAD NEA1120-05 Pin Puller | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Mass: 1.66 oz [47 g] MAX | on request |
| EBAD TiNi frangibolt | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Manufacturer: EBAD | on request |
| EBAD TiNi Micro Latch | Ensign-Bickford Aerospace & Defense (EBAD) | United States | — | on request |
| EH25 Bi-Axis Gimbal, 3-Phase | Sierra Space | United States | Motor type: 3-Phase (Enhanced Hybrid) | on request |
| Electric Lock | KOSMOLAB Launch Services | Russia | Dimensions (L×W×H): 48.7 × 37.4 × 22.4 mm | on request |
| Electro Mechanical Actuators (EMA) | AADYAH Aerospace | India | Variants: Linear and Rotary | on request |
| ELT M5 Mirror Support Cell — Precision Space Mechanism by SENER | SENER Aeroespacial | Spain | — | on request |
| EXOport | Exolaunch | Germany | Interface ports: 15" or 24" ESPA / SpaceX Dispenser Ring | on request |
| EXOtube | Exolaunch | Germany | Maximum satellite mass: 1000 kg | on request |
| Explosive Bolts | PacSci EMC | United States | Input stimulus, typical: 3.5 amp (when electrically initiated) | on request |
| FAULHABER GPT Planetary Gearheads | FAULHABER Drive Systems | Germany | Gearhead diameter: 22 ... 42 mm | on request |
| FB-2 Component Gear Set | Harmonic Drive | United States | Mass: 0.1 kg | on request |
| FB-32-157-2-GR Flat Component Set | Harmonic Drive | United States | Rated Torque L10: 82 Nm | on request |
| FBB Phasing Differential | Harmonic Drive | United States | Maximum Input RPM (Oil): 6000 | on request |
| FD-0A Phasing Differential | Harmonic Drive | United States | Mass(kg) 20: 2.0 | on request |
| FD-2A Differential Gear | Harmonic Drive | United States | Mass (Size 20): 0.6 kg | on request |
| FHA-C | Harmonic Drive | United States | Peak torque: 39~820 Nm | on request |
| FHA-C LW Mini | Harmonic Drive | United States | — | on request |
| FHA-Mini Actuator with Integrated Servo Drive | Harmonic Drive | United States | Supply Voltage Range: 24VDC Nominal +7 to 28VDC | on request |
| FHA-Mini Compact Hollow Shaft Servo Actuator | Harmonic Drive | United States | Maximum Torque (FHA-14C, 100): 28 N.m | on request |
| FLA Ultra-Flat Rotary Actuator | Harmonic Drive | United States | Gear Ratio (HP): 8, 9 | on request |
| Flexible Printed Circuits | Sheldahl (Multek Flexible Circuits) | United States | Circuit types: Single-sided, double-sided, multi-layer | on request |
| FlexRS® Category I | Large Space Structures GmbH | — | Applicable frequencies: up to Ka-band | on request |
| Fluid-Dynamic Attitude Control System (FDA) | ElmSpace | Germany | Technology: Fluid-dynamic attitude control | on request |
| FR-2 Pancake Gear | Harmonic Drive | United States | Gear Backlash: < 1.5 arc min | on request |
| Full Carbon Self-Deployable Booms | Prosix Engineering | Spain | Deployed length: Up to 28 m | on request |
| Gimbal and Actuator Controller Products | Data Patterns (India) Ltd. | India | — | on request |
| H25 Bi-Axis Gimbal, 4-Phase | Sierra Space | United States | Motor type: 4-Phase | on request |
| HarmonicGrease® | Harmonic Drive | United States | SK-1A Temperature: 0ºC to + 40ºC | on request |
| Harnesses | Hemeria | France | — | on request |
| HDRM REACT – Hold Down & Release Mechanisms (5KN, 15KN, 35KN) | Arquimea | Spain | Retention load variants: 5 kN, 15 kN, 35 kN | on request |
| HECTOR — SMA Rotary Actuator for Structural Deployment | Nimesis Technology | — | Technology: Shape memory alloy (SMA) rotary actuator | on request |
| Helical Rack and Pinion Gear Set | Harmonic Drive | United States | Helix angle: 19.5283° | on request |
| High-Precision Space Mechanisms | Swiss Centre for Electronics and Microtechnology (CSEM) | Switzerland | Precision: Micrometer-level, sub-micron resolution capable | on request |
| Hold Down Release Mechanism (HDRM) | Sierra Space | United States | Trigger mechanism: Redundant shape memory alloy (SMA) | on request |
| Honeycomb Sandwich Panels | Space Structures GmbH | Germany | Facesheet/core combinations: Aluminium/aluminium, GFRP/aluminium, CFRP/alum… | on request |
| HOTDOCK Mating/Demating Device | Space Applications Services | Belgium | Type: Mechanical mating/demating device | on request |
| HP3 Heat Probe Hammering Mechanism (NASA InSight) | Astronika | Poland | — | on request |
| HPG Harmonic Planetary® Precision Gearbox – Right Angle | Harmonic Drive | United States | Peak Torque: 150 Nm to 2,200 Nm | on request |
| HPG Planetary Gearbox | Harmonic Drive | United States | Peak Torque: 5 Nm to 3,200 Nm | on request |
| HPG-U1 Planetary Gear | Harmonic Drive | United States | Peak Torque: 5 Nm to 3,200 Nm | on request |
| HPGP Planetary Gearbox | Harmonic Drive | United States | Peak Torque: 12 Nm to 3,940 Nm | on request |
| HPN-A Planetary Gearbox | Harmonic Drive | United States | Peak torque: 9 Nm to 752 Nm | on request |
| HPN-L Planetary Gearbox | Harmonic Drive | United States | Peak torque: 9 Nm to 752 Nm | on request |
| IberEspacio Space Engineering and Systems Integration | Arquimea | Spain | Engineering disciplines: Thermal, propulsion, structures, RAMS, flight data… | on request |
| IFD100 Plug Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Connector model: IFD100 | on request |
| IFD200 Receptacle Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Connector model: IFD200 | on request |
| Intelligent Space Systems Interface (iSSI) | Skycorp Incorporated | United States | — | on request |
| intelligent Space Systems Interface Flight Qualification Experiment (iSSI FQE) | Skycorp Incorporated | United States | Launch vehicle/mission: NG-17 Cygnus (Northrop Grumman CRS-2) | on request |
| KDU Direct Drive | Harmonic Drive | United States | Maximum torque (KDU-13SB): 7.0 Nm (62.0 In.lb) | on request |
| KRAKEN Robotic Arm | Tethers Unlimited, Inc. (AMERGINT) | United States | Degrees of freedom: 7 DOF | on request |
| KSCS CubeSat Structure | Kairo Space | South Korea | Material: Aerospace-grade aluminum alloy | on request |
| LA Precision Linear Actuator | Harmonic Drive | United States | Max. driving force: 49 N (5kgf) | on request |
| Laser Scanning Actuator | Harmonic Drive | United States | Item/model: LSA-10A-30 | on request |
| LDC20 Low-Disturbance Gimbal | Sierra Space | United States | Configuration: Bi-axis, open-loop | on request |
| LEA Large Deployable Reflector Subsystems | HPS High Performance Space Structure Systems | — | Consortium role: LDRS-Prime (WeLEA consortium) | on request |
| Lighting Vision System | Kayser Space | Italy | — | on request |
| Lightweight 2-Axis Mini Gimbal | Sierra Space | United States | Configuration: X/Y 2-axis | on request |
| Linear Actuators | Moog Space Defense Group | United States | Actuator Model: 981* | on request |
| Liquid hydrogen tank | MT Aerospace | Germany | — | on request |
| Living Hinge Boom | Opterus Research and Development | United States | — | on request |
| Low-Cost Actuator 15 (LA15) | Beyond Gravity (ex-RUAG Space) | Switzerland | Motor type: Hybrid-type stepper motor with high detent torque | on request |
| MaalonDrive Rotary Micro-Positioning Drive | Micromotion GmbH | — | Sizes: 6 mm, 8 mm, 10 mm | on request |
| Mantis Capture Bag™ | TransAstra | United States | — | on request |
| Mars 2020 Perseverance Rover’s Primary Robotic Arm | Motiv Space Systems | United States | Payload: 45 kg (Earth gravity) | on request |
| memetis Microvalves | Memetis | — | Switching cycles (fatigue-free materials): Over 10 million | on request |
| memetis Microvalves & Microfluidic Systems | Memetis | — | Width: 5 mm | on request |
| Metallics | Tata Advanced Systems (Space) | India | — | on request |
| Mid-plane Standoff Kit | Pumpkin, Inc. | United States | Kit contents: 4 unique precision hard-anodized aluminum pieces + fastening … | $200 |
| Mirrored Panels | Media Lario | Italy | Weight per area: 15 kg/m2 | on request |
| Model 220 Rotary Actuator | Moog Space Defense Group | United States | Operating Voltage: 18 to 32 VDC | on request |
| Model 863 Rotary Actuator | Moog Space Defense Group | United States | Operating Voltage: 18 to 32 VDC | on request |
| Model 905 Rotary Actuator | Moog Space Defense Group | United States | Size: 2.3 x 4.9 x 5.4 inches | on request |
| Model 935 Rotary Actuator | Moog Space Defense Group | United States | Operating Voltage: 21 to 32 VDC | on request |
| Model 965 Rotary Actuator | Moog Space Defense Group | United States | Operating Voltage: 21 to 32 VDC | on request |
| Model 971 Rotary Actuator | Moog Space Defense Group | United States | Size: 3.0 x 3.48 x 6.56 inches | on request |
| Model 974 Linear Actuator | Moog Space Defense Group | United States | Size: 3.88 x 4.75 x 14.75 inches | on request |
| Modular CubeSat Structures | Serenum Space | Czech Republic | Material options: Aluminium Alloy, Stainless Steel Alloy, Titanium Alloy | on request |
| Modular Magnetic-Connector Satellite Platform | NazarX | Uzbekistan | Maintenance time reduction: several days to several hours | on request |
| ModuLink | Motiv Space Systems | United States | — | on request |
| Motion Controllers for DC Micro motors | FAULHABER Drive Systems | Germany | Voltage ranges - Motor: max. 30 V | on request |
| Multi-Purpose Actuators and Servoactuators | Moog Space Defense Group | United States | — | on request |
| Nano SmartPack Release Nut (nD3SP) | Dcubed | Germany | TRL: 9 | on request |
| Nanostruct 6U | GomSpace | Denmark | Default structure mass: 665 g | on request |
| NanoUtil FPP Top | GomSpace | Denmark | Dimensions: 98.0 mm x 98.0 mm x 8.5 mm | on request |
| NanoUtil FPP Top-S | GomSpace | Denmark | Operating temperature: -40…85 °C | on request |
| NanoUtil Interstage | GomSpace | Denmark | Supply voltage: 5 V | on request |
| NanoUtil Interstages GSSB | GomSpace | Denmark | Dimensions: 82.5 mm x 29.0 mm x (device dependent) | on request |
| NEA 1120-05 Pin Puller | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Mass: 47 g (1.66 oz) max | on request |
| NEA Hold Down Release Mechanisms | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Type: Non-Explosive Actuator (NEA) Hold-Down and Release Mechanisms | on request |
| NEA IFD100 Plug In-Flight Disconnect Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Shell size: 19 | on request |
| NEA IFD100 Plug In-Flight Disconnect Connector (Shell Size 25) | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Shell size: 25 | on request |
| NEA IFD200 Receptacle In-Flight Disconnect Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Shell size: 19 | on request |
| NEA IFD200 Receptacle In-Flight Disconnect Connector (Shell Size 25) | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Shell size: 25 | on request |
| NEA ZSF100 Plug Zero Separation Force Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Shell size: 21 | on request |
| NEA ZSF100/200 Zero Separation Force & In-Flight Disconnect (IFD) Electrical Interconnect | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Separation force: 0 N (0 lbf) (or adjustable to customer spec) | on request |
| NEA ZSF100P Plug Zero Separation Force Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Shell size: 17 | on request |
| NEA ZSF200 Receptacle Zero Separation Force Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Shell size: 21 | on request |
| NEA ZSF202S Receptacle Zero Separation Force Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Shell size: 25 | on request |
| NEA® Model 9104 Hold Down & Release Mechanism (HDRM) | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Proof load rating: 18,750 lbf (84,000 N) | on request |
| OHP Chassis | Thermavant | United States | Simple chassis example thermal performance (OHP): 11 °C rise per 120 W | on request |
| OHP Heat Frames | Thermavant | United States | 3u example thermal performance (OHP): 10 °C rise per 130 W | on request |
| On-Orbit Robotic Servicing System | DeltaV Robotics | United States | Technology: Autonomous robotic arm, end-effectors, AI vision and pose estim… | on request |
| OneCatch™ | Enduralock | United States | Actuators: 3 | on request |
| Orbital S Multi-Robot 3D Printer | Orbital Composites | United States | — | on request |
| OrbShield™ | Orbital Composites | United States | Standard size: 1U | on request |
| PEEK CubeSat Structures | Lamb Space Tec | Poland | Stroke: Max. 4.5 mm | on request |
| Phase Adjusters | Harmonic Drive | United States | Torque range: 500 in-lb to 20,000 in-lb | on request |
| phySPACE Schrittmotoren für Weltraumanwendungen | Phytron GmbH | Germany | — | on request |
| phySPACE Stepper Motors for NASA’s CLPS Initiative | Phytron GmbH | Germany | — | on request |
| PIAP Space Robotic Manipulator Systems | PIAP Space | Poland | Products: Robotic manipulator arms and mechanisms | on request |
| Plan-S (Connecta) Satellite Deployable Structures | Plan-S (Connecta) | Turkey | Products: Deployable structures, solar panel and antenna deployment mechanisms | on request |
| PocketQube Satellite Structure | Tetonsys | United States | Form factors: 1P, 2P, 3P PocketQube | on request |
| Precision Assemblies | Space Structures GmbH | Germany | In-house processes: Bolting, riveting, bonding, alignment, measurement | on request |
| Precision Component Sets | Harmonic Drive | United States | Accuracy: <1 arc-min | on request |
| Precision Manufacturing and Engineering Services | Sidus Space, Inc. | United States | Flight heritage: Over 20 years | on request |
| Precision Missile Actuation Systems | Moog Space Defense Group | United States | — | on request |
| Pridwen Heatshield | Space Forge Limited | United Kingdom | Design: Non-ablative, shuttlecock-style deployable heat shield | on request |
| Printer Assisted Deployment System (PADS) | Orbital Matter | Poland | Boom length: 10 meters to over 100 meters | on request |
| Prusament PC Space Grade Black | TRL Space | Czech Republic | Tensile strength: 75 MPa | on request |
| RadShield — Radiation Shielding Technology | TakeMe2Space | India | Substrate material: 2 mm thick Aluminium AL 6061 | on request |
| RasuunDrive Linear Spindle Drive | Micromotion GmbH | — | Drive type: Linear spindle drive | on request |
| REL Servo Drive | Harmonic Drive | United States | Command Interface: CANopen over EtherCAT (CoE), ASCII and discrete I/O, Ste… | on request |
| Release Nuts | Dcubed | Germany | Dimensions (SmartPack Release Nut nD3SP): 74x35x4 mm / 2.91x1.38x0.16 in | on request |
| Remove-Before-Flight (RBF) Bracket Kit | Pumpkin, Inc. | United States | Material: Al 5052-H32, plated per CubeSat Design Specification (CDS) | $165 |
| Remove-Before-Flight (RBF) Pin and Lanyard | Pumpkin, Inc. | United States | SKU: 710-00300 | $70 |
| Resolver für VSS Schrittmotoren der Baugrößen 25 bis 126 | Phytron GmbH | Germany | — | on request |
| RH Mini Actuator | Harmonic Drive | United States | Mass: 0.09 kg (RH-5A) | on request |
| RIDDANCE | Orbotic Systems | United States | — | on request |
| RKF Actuator | Harmonic Drive | United States | Mass (RKF-20A): 2.9 kg | on request |
| Roccor Deployable Booms and Solar Array Structures | Roccor (Redwire) | United States | Products: Deployable booms, solar array structures, antenna mechanisms | on request |
| Rod & Spacer Kit | Pumpkin, Inc. | United States | Mass: 4 g | on request |
| Rotary Actuators | Moog Space Defense Group | United States | Load Torque: 25 to 2,500 in-lb | on request |
| RSF Actuator | Harmonic Drive | United States | Rated Output (RSF-17A, Ratio 50): 62 W | on request |
| RSF-Mini | Harmonic Drive | United States | Model: RSF-8B, RSF-11B, RSF-14B | on request |
| RSF-Supermini Brushless Servo Actuator | Harmonic Drive | United States | Rated Torque (RSF-3C, 30): 0.03 Nm | on request |
| SARA21 General Purpose Rotary Actuator | Beyond Gravity (ex-RUAG Space) | Switzerland | Units in space: More than 110; first flight 2005 | on request |
| Satellite Structure Assembly and Integration | Tata Advanced Systems (Space) | India | Products: Composite structures, metallic components, spacecraft assembly | on request |
| Satellite Structure Panels | Beyond Gravity (ex-RUAG Space) | Switzerland | Panel construction: Honeycomb panels with aluminium or carbon-reinforced fa… | on request |
| SATLATCH — Rotary Deployment and Latching Mechanism | Nimesis Technology | — | Technology: CuAlNi shape memory alloy rotary mechanism | on request |
| Sentinel-2 Satellite Structure | Beyond Gravity (ex-RUAG Space) | Switzerland | — | on request |
| SEPTA36 Solar Array Drive Mechanism | Beyond Gravity (ex-RUAG Space) | Switzerland | Type: Solar Array Drive Mechanism (high power class) | on request |
| SEPTA36G Solar Array Drive Mechanism | Beyond Gravity (ex-RUAG Space) | Switzerland | Type: Solar Array Drive Mechanism (high power class, demanding missions) | on request |
| SEPTA42 Solar Array Drive Mechanism | Beyond Gravity (ex-RUAG Space) | Switzerland | Target application: Small satellites and constellations | on request |
| Servo Drives | Harmonic Drive | United States | Power: 4 kW | on request |
| Servo Mount Gearheads | Harmonic Drive | United States | Planetary Gearbox backlash (standard): < 3 arc-min | on request |
| SHA Integrated with Servo Drive | Harmonic Drive | United States | Maximum torque: 68-477 Nm | on request |
| SHD-2SH Hollow Shaft Gear | Harmonic Drive | United States | Rated Torque L10: 3.7 Nm | on request |
| SHD-2UH Lightweight Gear Unit | Harmonic Drive | United States | Accuracy: <1 arc-min (most sizes) | on request |
| SHF-11-50-2UH Hollow Shaft Gear Unit | Harmonic Drive | United States | Mass: 0.53 kg | on request |
| SHF-2A Component Set | Harmonic Drive | United States | Peak torque: 9 ~ 1800 N•m | on request |
| SHG-50-100-2UJ Gear Unit | Harmonic Drive | United States | Rated Torque L10: 611 Nm | on request |
| SINGLE LAYER MEASURING BELLOWS | Saransk Instrument-Making Plant | — | Purpose: Single layer metal measuring bellows are intended for operation as… | on request |
| Six-Axis CubeSat Boom Deployer | CTD (Composite Technology Development) | United States | Deployed span: 6.0 m tip-to-tip about three axes | on request |
| Slip Rings for Space Applications | Beyond Gravity (ex-RUAG Space) | Switzerland | Product families: SADA/SADM slip rings, payload slip rings, limited angular… | on request |
| SM CubeSat Structures | NPC Spacemind | — | Sm01 dimensions (w/o kill switches): 113.5 x 100.0 x 100.0 mm, 1U, up to 6 … | on request |
| SM01 | NPC Spacemind | — | Structure size: 1U CubeSat | on request |
| SM02 | NPC Spacemind | — | Form factor: 2U Cubesat Structure | on request |
| SM03 | NPC Spacemind | — | Structure: 3U CubeSat Structure | on request |
| SM04 | NPC Spacemind | — | CUBESAT structure: 4U | on request |
| SM06 | NPC Spacemind | — | CUBESAT structure: 6U | on request |
| SM08 | NPC Spacemind | — | CUBESAT structure: 8U | on request |
| SM12 | NPC Spacemind | — | CUBESAT structure: 12U | on request |
| SM16 | NPC Spacemind | — | CUBESAT structure size: 16U | on request |
| Solar Array Drive Assembly (SADA) | Shenzhen MagicCubeSat Technology (MCS) | China | Function: Solar array pointing drive | on request |
| Solar Panel Clips Set for AntS antenna | Pumpkin, Inc. | United States | Thickness: 0.031"/0.8 mm | $395 |
| Space Mechanisms (SADA, Gimbals, Rotary Actuators) | Moog Space Defense Group | United States | Sada — type 3/5: Single-axis solar array drive; 40+ year heritage | on request |
| Space Mechanisms and Solar Array Systems | SENER Aeroespacial | Spain | Products: Solar array drives (SADM), antenna pointing mechanisms (APM), hol… | on request |
| Space Robotics and In-Space Assembly | GITAI | Japan | Robot: S2 robotic arm — force-sensing, teleoperated, general-purpose | on request |
| Spacecraft Mechanisms and Deployment Systems | Froberg Aerospace | United States | Products: Deployment actuators, hold-down releases, antenna pointing drives… | on request |
| Spacecraft Structures | AstroForge | United States | Vehicle Mass (DeepSpace-2): 200 kg | on request |
| SpaceStrut Struts and Booms | Space Structures GmbH | Germany | Hybrid strut construction: Composite tube (filament winding, thermoplastic,… | on request |
| Spartan Space EuroHab/ILOT — Inflatable Lunar Habitat | TechTheMoon | France | Type: Inflatable lunar habitat | on request |
| Speed Controllers | FAULHABER Drive Systems | Germany | PWM switching frequency: 96 kHz | on request |
| Stand-Off Mechanism (SOM) | MMA Design | — | Deployed height: ~8 inches | on request |
| Structure 1U CubeSat with Separation System | SPUTNIX | Russia | Year of release: 2017 | on request |
| Structures | Hemeria | France | Structures designed per year: 400 | on request |
| SUPERNOVA™ Structural Components | Pumpkin, Inc. | United States | — | on request |
| Tanks in Space | MT Aerospace | Germany | — | on request |
| Tanques soldados por Friction Stir Welding (FSW) | VENG S.A. | Argentina | Prototype tank length: 3.5 m | on request |
| Thermal Strap / Thermal Link | Azimut Space | Germany | — | on request |
| ThinkToolkit | ThinkOrbital, Inc. | United States | Welding method: Electron beam welding | on request |
| TiNi ERM E1000 Ejector Release Mechanism | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Max release load: 1,000 lbf (4,448 N) | on request |
| TiNi ERM E2000 Ejector Release Mechanism | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Max release load: 2,000 lbf (8,900 N) | on request |
| TiNi ERM E250 Ejector Release Mechanism | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Max release load: 250 lbf (1,112 N) | on request |
| TiNi ERM E4000 Ejector Release Mechanism | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Max release load: 4,000 lbf (17,800 N) | on request |
| TiNi ERM E500 Ejector Release Mechanism | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Max release load: 500 lbf (2,224 N) | on request |
| TiNi Flat Pack FP50 Frangibolt Actuator | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Mass: 1.17 oz (33 g) max | on request |
| TiNi Frangibolt Actuator FB12 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Ti fastener size: 1" | on request |
| TiNi Frangibolt Actuator FC2 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Ti fastener size: #8 | on request |
| TiNi Frangibolt Actuator FC3 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Ti fastener size: #10 | on request |
| TiNi Frangibolt Actuator FC4 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Ti fastener size: 1/4" | on request |
| TiNi Frangibolt Actuator FC6 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Ti fastener size: 3/8" | on request |
| TiNi Frangibolt Actuator FC8 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Ti fastener size: 1/2" | on request |
| TiNi MINI Frangibolt FD04 Actuator | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Ti fastener size: #4 | on request |
| TiNi Pin Puller P10 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Pull force: 10 lbf (44 N) | on request |
| TiNi Pin Puller P100 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Pull force: 100 lbf (445 N) | on request |
| TiNi Pin Puller P1000 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Pull force: 1,000 lbf (4,450 N) | on request |
| TiNi Pin Puller P25 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Pull force: 25 lbf (111 N) | on request |
| TiNi Pin Puller P5 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Pull force: 5 lbf (22 N) | on request |
| TiNi Pin Puller P50 | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Pull force: 50 lbf (222 N) | on request |
| TITAN — 7-DOF Orbital Robotic Arm | PIAP Space | Poland | Degrees of freedom: 7 | on request |
| Toray TC380 Epoxy Prepreg | Toray Industries Space | Japan | Resin system: Epoxy (TC380) | on request |
| Unidirectional Tapes | Sheldahl (Multek Flexible Circuits) | United States | Product forms: Unidirectional reinforcement tapes, coated tapes, adhesives/… | on request |
| VACCO F1D10286-02 etched disc filter | VACCO Industries | United States | Materials of construction: Titanium alloy | on request |
| VACCO F1D10588-01 Etched Disc Filter | VACCO Industries | United States | Materials of construction: Titanium alloy | on request |
| VACCO F1D10636-01 Etched Disc Filter | VACCO Industries | United States | Materials of construction: CRES 304L | on request |
| VACCO F1D10638-01 Etched Disc Filter | VACCO Industries | United States | Materials of construction: Titanium alloy | on request |
| VACCO F1D10639-01 Etched Disc filter | VACCO Industries | United States | Materials of construction: CRES 304L | on request |
| VACCO F1D10784-01 etched disc filter for Xenon application | VACCO Industries | United States | Materials of construction: Titanium alloy | on request |
| VACCO F1D10807-02 Etched Disc Filter | VACCO Industries | United States | Materials of construction: Titanium alloy | on request |
| Vega-C Payload Fairing | Beyond Gravity (ex-RUAG Space) | Switzerland | — | on request |
| VERSE CubeSat Structures | 2NDSpace Srl | Italy | Verse-01 form factor: 1U, mass 90 g | on request |
| xLink™ System | Motiv Space Systems | United States | Modularity: Building block approach for customization | on request |
| ZAPHOD CubeSat Structure | AAC Clyde Space | Sweden | TRL: 9 | on request |
| Zeus Modular Payload Adapter | Deployable Space Systems (DSS) — now Redwire | United States | Dimensions (STOWED): 1575 mm interface to PAF | on request |
| ZSF100 Plug Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Connector model: ZSF100 | on request |
| ZSF100P Plug Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Connector model: ZSF100P | on request |
| ZSF200 Receptacle Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Connector model: ZSF200 | on request |
| ZSF202S Receptacle Connector | Ensign-Bickford Aerospace & Defense (EBAD) | United States | Connector model: ZSF202S | on request |
Products
Products by manufacturer
2NDSpace Srl
Italy · 2023 · 1 productNew Space company designing modular nanosatellite/CubeSat hardware: structures, solar panels, EPS, antennas, OBCs, and deployers/separation systems.

VERSE CubeSat Structures
Modular CubeSat structures from 1U to 16U with flight-proven reliability and fully customizable interfaces.
| Verse-01 form factor | 1U, mass 90 g |
| Verse-02 form factor | 2U, mass 195 g |
| Verse-03 form factor | 3U, mass 290 g |
| Verse-06 form factor | 6U, mass 690 g |
| Verse-08 form factor | 8U, mass 890 g |
AAC Clyde Space
Sweden · 1999 · 1 productAAC Clyde Space provides small satellite technologies and space-based data services, offering end-to-end solutions from satellite components to data analytics for various applications.

ZAPHOD CubeSat Structure
The ZAPHOD CubeSat Structure range offers lightweight, robust, and user-friendly structures for CubeSats, available in 3U, 6U, and other form factors.
| TRL | 9 |
| Flown since | 2014 |
| Form factors | 3U, 6U & other form factors |
| Compliance | CubeSat design specification |
| Compatibility | All rail-deployers, manned flights, ISS |
AADYAH Aerospace
India · 1 productAerospace company supporting space exploration missions; partners with ISRO, Skyroot, Orbex, Bellatrix, and Latitude on lunar and Mars programmes.

Electro Mechanical Actuators (EMA)
Linear and rotary electro-mechanical actuators for aerospace and defense — replaces hydraulic/pneumatic actuation, AS9100D certified, for rockets, missiles, UAVs, and aircraft.
| Variants | Linear and Rotary |
| Control type | Fly-by-wire compatible |
| Applications | Defense aircraft, jet fighters, rockets, missiles, UAVs |
| Quality standard | AS9100D certified |
ACT (Advanced Cooling Technologies)
United States · 2003 · 1 productPremier thermal management solutions company specializing in custom two-phase heat transfer technology for aerospace, defense, and industrial applications.

Composite Structures and Assemblies
Advanced composite structural solutions for space and aerospace applications including spacecraft bus structures, solar array substrates, booms, and support structures with maximum
| Manufacturing process | 5-axis CNC machining, autoclave cure, aerospace-grade bonding |
| Material systems | CFRP, aluminum honeycomb, hybrid composites |
| Applications | Bus structures, payload structures, solar array substrates, booms |
| Quality certification | AS9100D |
Adaptive Launch Solutions
United States · 2010 · 1 productAdaptive Launch Solutions (ALS) provides launch integration services and designs adaptive structures and avionics for multi-manifesting pico to small satellites on various launch vehicles.

A-Deck Adapter System
TRL-8 spacecraft adapter system rated to 1,000 kg supporting Pico through Mini class satellites as hosted or secondary payloads on EELV launch vehicles.
| TRL | 8 |
| Rated capacity | 1,000 kg |
| Compatible vehicles | EELVs |
| Supported satellite classes | Pico, Nano, Micro, Mini |
Alba Orbital
United Kingdom · 2012 · 5 productsAlba Orbital manufactures PocketQube satellites, provides launch and ground station services, and operates a fleet of nighttime imaging satellites for government and commercial clients.

1P Skeleton Wall PocketQube Structure
A skeletonized aluminum structure designed for 1P PocketQube pico-satellites, featuring access points for internal electronics and compatibility with PQ60 v1.0 board stacks.
| Dimensions | 1P (Unit) - 50 mm x 50 mm external dimensions. 47 mm x 47 mm internal dimensions (widest p |
| Flight heritage | Earlier version has Flight Heritage |
| Mass | 0.069 kg |
| Internal volume | 1.09 10-4 m3 |
| Static load | >± 392.4 m/s2 |

2P Skeleton Wall PocketQube Structure
A skeletonized wall structure designed for the PocketQube Standard (Pico-satellite class), made from aerospace-grade aluminum.
| Dimensions | 2P (Unit) |
| External dimensions | 114 mm x 50 mm x 50 mm |
| Internal dimensions (widest point) | 114 mm x 47 mm x 47 mm |
| Manufacturer | Alba Orbital |
| Flight heritage | Earlier version has Flight Heritage |

3P Skeleton Wall PocketQube Structure
The 3P Skeleton Wall PocketQube Structure is an aerospace-grade aluminum structure designed for the PocketQube Standard (Pico-satellite class), featuring double redundancy kill swi
| Dimensions | 3P (Unit) |
| External dimensions | 178 mm x 50 mm x 50 mm |
| Internal dimensions (widest point) | 178 mm x 47 mm x 47 mm |
| Manufacturer | Alba Orbital |
| Lead time | 8 weeks depending on available stock levels (much sooner if in stock) |

Bundle (1p,1.5p,2p,2.5p) Skeleton Wall PocketQube Structures
A bundle of four Skeleton Wall PocketQube satellite structures (1p, 1.5p, 2p, 2.5p sizes), one of each, designed for the PocketQube femto-satellite standard.
| Dimensions | 1p,1.5p,2p,2.5p (Unit) |
| Price | £9,999.00 |
| Lead time | 4 weeks depending on available stock levels (much sooner if in stock) |
| Datasheet/brochure | Coming Soon |

Custom PocketQube Structural Panel
A custom structural panel for PocketQubes, designed to accommodate unique payloads requiring non-standard access points to the end wall of the structure.
| Dimensions | 1p/1.5p/2p/3p |
Aphelion Orbitals
United States · 2017 · 1 productAphelion Orbitals is a New Jersey-based launch vehicle company developing the Helios nanosatellite launch system for regular, scheduled orbital access at low cost.

1U Cubesat Structure
The Aphelion 1U structure is an open frame, lightweight CubeSat structure made from 7075 aluminum, designed for easy configuration and access during development.
| Height | 113.5 mm |
| Width | 100 mm |
| Depth | 100 mm |
| Material | 7075-T651 |
| Mass | 92 g |
Arquimea
Spain · 2007 · 3 productsSpanish space technology company founded 2007 in Leganes, developing MEMS relay switches, SiC power devices, and miniaturized power conditioning units for satellite applications.

Deployment Mechanisms for Satellites (Solar Arrays, Antennas & Instruments)
Hinge- and spring-based deployment mechanisms with integrated deployment detection for satellite solar arrays, antennas, and instruments, offered as off-the-shelf or custom solutio
| Reference application | 1 × 1 m solar array release and deployment mechanism |
| Overall system mass (reference config) | 560 g (including screws and harness) |
| Operating temperature | -40°C to +100°C |
| Solar panel stowed separation | 20 mm from spacecraft to panel |
| Deployment detection | Sensor detects start and end of deployment |

HDRM REACT – Hold Down & Release Mechanisms (5KN, 15KN, 35KN)
Space-qualified, non-explosive, in-field resettable Hold Down & Release Mechanisms in 5KN, 15KN and 35KN variants based on Shape Memory Alloy (SMA) technology for satellite pay
| Retention load variants | 5 kN, 15 kN, 35 kN |
| Release shock level | <1300 g's at maximum load |
| Operation temperature range | -90°C to +125°C |
| Actuation temperature options | Up to +65°C and up to +125°C |
| SMA motorization options | TiNi or SMARQ® Shape Memory Alloy |
IberEspacio Space Engineering and Systems Integration
Multi-discipline spacecraft engineering services — thermal analysis, xenon pressure regulators, structural integration (SpaceIL Beresheet lunar lander structure), RAMS, and in-orbi
| Engineering disciplines | Thermal, propulsion, structures, RAMS, flight data analysis |
| Propulsion products | Xenon electronic pressure regulators, propellant management units |
| Structural heritage | SpaceIL Beresheet lunar lander primary structure (launched February 2019) |
| Thermal analysis capability | Custom thermal software libraries, vacuum simulation, TMM development and correlation |
| Gse | Custom ground support equipment design and supply |
Astrix Astronautics
New Zealand · 2017 · 1 productAstrix Astronautics provides inflatable space deployment systems for solar arrays, radiators, antennas, drag sails, and heat shields, offering high surface area and mass efficiency.

Astrix Inflatable Deployment System
The Astrix Inflatable Deployment System provides a highly efficient and mass-effective solution for deploying large surface areas in space, enabling applications like solar arrays,
| Deployment efficiency (space) | 20x more space efficient |
| Deployment efficiency (mass) | 4x more mass efficient |
| Deployable area increase | 20x |
| Solar array power (Copia) | up to 300 watt/kg |
| Flight heritage | Yes |
AstroForge
United States · 2022 · 2 productsAstroForge is a deep-space mining company that builds spacecraft to track and extract valuable metals from asteroids, aiming to integrate space resources into Earth's supply chain.

Asteroid Refinery Technology
AstroForge's in-space metallurgical refining technology for processing platinum group metal ore extracted from asteroids directly in orbit.
| Target metals | Platinum group metals (Pt, Pd, Ir, Rh, Os, Ru) |
| Process | In-space pyrometallurgical/hydrometallurgical refining |
| Processing location | Asteroid orbit (in-situ processing before Earth return) |
| Return method | Reentry capsule (refined metal ingots) |
| Terrestrial pgm grade | <1 ppm (Earth crust average) |

Spacecraft Structures
AstroForge's spacecraft structures are designed to support, deploy, protect, and correctly orient various equipment and instrumentation, ensuring hardware survives launch and funct
| Vehicle Mass (DeepSpace-2) | 200 kg |
| Axial Load Factor (DeepSpace-2) | 8.0g |
| Lateral Load Factor (DeepSpace-2) | 12.5g |
| Bolt Circle for Mounting | 24 inch |
| Propellant Tank Mass | 11 kg |
Astronika
Poland · 2013 · 1 productAstronika is a Polish space mechanisms company and ESA/NASA mission supplier, developing deployable booms, hold-down mechanisms, penetrating devices, and precision actuators for science and commercial satellite missions.

HP3 Heat Probe Hammering Mechanism (NASA InSight)
Astronika is a Polish space engineering company specializing in miniaturized space mechanisms including penetrators, deployable booms, and hammering systems. For NASA’s InSig
Astroscale US
Japan · 1 productPioneer in space debris removal and satellite life extension services, developing rendezvous, proximity operations, and capture technologies to ensure sustainable orbital environments.

Docking Plate
A flight-proven, commercially available standardized docking interface that satellite operators install on their spacecraft to enable access to Astroscale's full suite of on-orbit
| Generation | Second generation (flight-proven) |
| Availability | Off-the-shelf, commercially available |
| Installation | 3-bolt solution, assemblable from outside the spacecraft |
| Capture compatibility | Magnetic and robotic grappling mechanisms |
| Thermal design | De-coupled top plate and structural deck |
Azimut Space
Germany · 2007 · 1 productAzimut Space GmbH is a Berlin-based space engineering SME with 15+ years of experience in thermo-mechanical engineering, developing thermal control systems, payloads, scientific instruments, and ground support equipment for satellite, instr

Thermal Strap / Thermal Link
Custom flexible thermally conductive links made of copper, aluminium, or Pyrolytic Graphite Sheets for precise heat management in space applications.
Beyond Gravity (ex-RUAG Space)
Switzerland · 1993 · 11 productsSwiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.

APPMAX2 Electric Propulsion Pointing Mechanism
Low-cost, easy-to-integrate 2-axis thruster gimbal for electric propulsion, supporting 1 to 5 kW thrusters within a 15 degree pointing cone.
| Axes | 2-axis pointing mechanism |
| Thruster power range | 1 to 5 kW |
| Pointing range | 15 degree cone |
| Integration | Simple integration without zero gravity devices |
| Variants | APPMAX2-H (50 kg thruster, with hold-down and release mechanism), APPMAX2-S (downscaled, i |

APPMAX3 Deployable Thruster Pointing Mechanism
Modular deployable 3-axis thruster gimbal driven by three stepper-motor actuators, with micrometeorite-shielded piping and zero-G device.
| Actuation | Three stepper motor-based actuators |
| Configuration | Modular deployable thruster mechanism with robotic arm deployment |
| Protection | Micrometeorite shielding on piping; thermal and micrometeorite protection for actuators |
| Thermal control | Flow controller with radiators and/or MLI per thermal analysis |
| Mounting | Direct hard mounting baseline; elastomer dampers optional |

Low-Cost Actuator 15 (LA15)
Hybrid stepper actuator with high unpowered detent torque, planetary gear and high-load output bearings for electric propulsion pointing mechanisms.
| Motor type | Hybrid-type stepper motor with high detent torque |
| Gear | Planetary gear |
| Bearings | High-load output bearings |
| Unpowered behaviour | High unpowered detent torque; holds pointing position under high back-driving torques |
| Design basis | Beyond Gravity modular actuator system |

SARA21 General Purpose Rotary Actuator
Compact, back-drivable general purpose rotary actuator with more than 110 units in space since 2005 and a simple stepper motor interface.
| Units in space | More than 110; first flight 2005 |
| Production capacity | Up to 50 units per year; in continuous production for 20 years |
| Interface | Simple stepper motor interface |
| Mechanical | High torque capacity, safely back-drivable |
| Typical application | Antenna pointing (other applications possible) |

Satellite Structure Panels
High-performance honeycomb panels with aluminium or carbon-reinforced face sheets, produced on an industrialized line including a US site in Titusville.
| Panel construction | Honeycomb panels with aluminium or carbon-reinforced face sheets |
| Configurable parameters | Panel thickness, face sheet material, core density |
| Production sites | Includes highly automated US site in Titusville, Florida |
| Insert technology | Automated potting of patented GreDom inserts |
| Flight heritage | Over 650 OneWeb satellites |
Sentinel-2 Satellite Structure
RUAG Space (now Beyond Gravity) is one of Europe’s leading suppliers of satellite structures and payload fairings. For the ESA Copernicus Sentinel-2 Earth observation satelli

SEPTA36 Solar Array Drive Mechanism
Fully qualified high-power Solar Array Drive Mechanism from Beyond Gravity's modular SADM family, qualified for LEO and GEO missions.
| Type | Solar Array Drive Mechanism (high power class) |
| Qualification | Fully qualified; qualified for LEO and GEO missions |
| Slip ring | In-house gold-on-gold slip ring technology |
| Modularity | Interfaces remain the same regardless of power class |
| Assembly | Actuator part, slip ring with connectors, customizable solar array connectors, motor and s |

SEPTA36G Solar Array Drive Mechanism
Fully qualified Solar Array Drive Mechanism variant of the modular SEPTA family for demanding missions.
| Type | Solar Array Drive Mechanism (high power class, demanding missions) |
| Qualification | Fully qualified; qualified for LEO and GEO missions |
| Slip ring | Flight proven in-house slip ring technology |
| Modularity | Interfaces remain the same regardless of power class |
| Assembly | Actuator part, slip rings with connectors, customizable solar array connectors, motor and |

SEPTA42 Solar Array Drive Mechanism
Constellation SADM for small satellites, produced at up to 18 units per month with more than 100 flight models already delivered.
| Target application | Small satellites and constellations |
| Production rate | Up to 18 units per month |
| Units delivered | More than 100 flight models |
| Qualification status | TRL8 completed for all variants; TRL9 by projected launch end of 2025 |
| Power transfer options | One or two gold-on-gold slip rings, or cable wrap |

Slip Rings for Space Applications
Custom and modular space slip rings for solar array drives, payloads and limited-angle actuators, with over 2,000 cumulative years of flight time.
| Product families | SADA/SADM slip rings, payload slip rings, limited angular rotational actuator slip rings |
| Modular ranges | C-Series cylindrical modules, P-Series planetary modules (stackable) |
| Power classes | Below 3 kW to above 30 kW |
| Contact technology | Gold-on-gold |
| Flight heritage | Over 2,000 cumulative years of flight time; 100% mission success rate |
Vega-C Payload Fairing
Beyond Gravity (formerly RUAG Space, rebranded in 2022) designs and manufactures payload fairings for European launch vehicles. For Vega-C, Beyond Gravity delivers the 2.6-metre di
Boltless CubeSat Structures (Kikuchiseiki, KIKUCHI SEIKI)
Japan · 1961 · 1 productKikuchi Seiki provides high-precision metalworking services, including machining, fabrication, and assembly, specializing in components for various industries, including aircraft engines.

CubeSat Structures (Boltless Structure)
Kikuchi Seiki offers CubeSat structures, including a unique boltless design, along with development and machining services for space applications.
| Structure type | Boltless Structure |
| Fastening | No Fastening |
| Performance and reliability | Ensured High Performance and Reliabilities for Space Applications |
| Precision of rails | 50 μm (for 3U and 6U) |
Comat
France · 1963 · 1 productComat is a French aerospace equipment manufacturer, part of the Hemeria group, designing flight hardware and mechanisms for small satellites, telecommunications/observation payloads, and space exploration missions.
3POD
The 3POD is an antenna-pointing mechanism designed for X-band telemetry downlink on next-generation Earth Observation satellites, orienting a Ø220 mm high-gain parabolic X-band ant
| Pointing accuracy | 1° (worst case) |
| Slew rate | 5°/s |
| Elevation range | +/-74° |
| 90° rotation time | <15 s |
| Rotation time (average) | 8 s |
Compoxi
Spain · 4 productsCompoxi is a Spanish composite design and manufacturing company delivering turnkey carbon-fiber and glass-fiber structures for space, aeronautics, and industrial applications, including satellite structures, radomes, antennas, and solar arr
Composite Radomes for Launchers and Satellites
Glass-fiber reinforced polymer (GFRP) radomes manufactured for European launch vehicles and for LEO/GEO orbit satellites.

Compoxi
Compoxi is a composite design and manufacturing company delivering turnkey CFRP/GFRP structural components for the space sector, including radomes, satellite structures, antennas a

Compoxi Space Composite Manufacturing
Turnkey composite design and manufacturing services for space applications, including radomes, satellite structures, antennas, HAPS structural elements and solar array substrates.
| Products delivered to orbit | 850 |

Compoxi Space Composite Structures & Components
Custom composite (GFRP/CFRP) design and manufacturing services for space applications, including radomes, satellite structures, antennas, HAPS structural elements and solar array s
CTD (Composite Technology Development)
United States · 1988 · 4 productsCTD develops state-of-the-art composites for extreme conditions and demanding applications in aerospace, high performance magnets, cryogenic systems, marine, automotive, and industrial sectors.

1U Quad CubeSat Boom Deployer
1U CubeSat boom deployer carrying four booms with wire management, deploying to 3.0 m.
| Form factor | 1U CubeSat |
| Booms | Four (quad), with wire management |
| Deployed length | 3.0 m |
| Boom construction | Overlapping slit-tube booms, or patented Slit-Lock for maximum payload stability |
| Boom material - carbon fibre composite | Ultimate stiffness and thermal stability |

Composite Spacecraft Structures and Booms
Composite Technology Development's (CTD) carbon fiber reinforced polymer spacecraft booms, solar array substrates, antenna reflectors, and precision space structures.
| Products | Composite booms, solar array substrates, antenna reflectors, structural panels |
| Boom types | Deployed by spring (bistable) or motorized; self-deploying shape-memory variants |
| Material | CFRP (carbon fiber reinforced polymer), graphite/cyanate ester, M55J/RS-3 |
| Cte | Near-zero CTE achievable for dimensionally stable optical structures |
| Customers | JPL, NASA Goddard, commercial satellite OEMs |

CTD Composite Deployable Structures
Composite Technology Development produces deployable composite booms, solar array structures, and antenna reflectors for spacecraft.
| Products | Deployable booms, solar array structures, antenna reflectors |
| Material | High-stiffness composite materials |

Six-Axis CubeSat Boom Deployer
Patented multi-axis CubeSat boom deployer with a 6.0 m tip-to-tip deployed span about three axes.
| Deployed span | 6.0 m tip-to-tip about three axes |
| Boom construction | Overlapping slit-tube booms, or patented Slit-Lock for maximum payload stability |
| Boom material - carbon fibre composite | Ultimate stiffness and thermal stability |
| Boom material - fiberglass | RF transparency |
| Boom material - hybrid metal-composite | Antenna elements |
CubeSat Aerospace
India · 3 productsIndian CubeSat developer offering flight-ready 1U–6U satellite structures, subsystem components, environmental testing services, launch integration, and STEM education programs from Ahmedabad.

1U CubeSat Structure
An aerospace-grade 1U CubeSat structure designed for durability, easy integration, and industry compliance, supporting major deployers and subsystems for research and commercial mi
| Dimensions | 100 mm × 100 mm × 113.5 mm |
| Mass | ~1.33 kg |
| Material | Aerospace-grade aluminum (6061-T6 or equivalent) |
| Rail system | Anodized aluminum for reduced friction during deployment |
| Structural features | Corner fasteners, precision-aligned mounting holes |

CubeSat Aerospace Satellite Structures (1U–6U)
Aerospace-grade aluminum 6061-T6 CubeSat structures from 1U to 6U — certified to ISO 9001:2015, NASA GEVS, MIL-STD-810G, ESA ECSS; P-POD/ISIPOD compatible.
| 1u dimensions | 100 × 100 × 113.5 mm |
| 1u mass | ~1.33 kg |
| 1.5u dimensions | 100 × 100 × 170.25 mm |
| 2u dimensions | 100 × 100 × 227 mm |
| 3u dimensions | 100 × 100 × 340.5 mm |

CubeSat Transporter
The CubeSat Transporter by CubeSat Aerospace is a rugged, reusable container designed to protect CubeSats during storage, shipping, and handling, accommodating 1U to 3U structures
| Supported sizes | 1U, 1.5U, 2U, and 3U CubeSats (interchangeable inserts) |
| Outer dimensions | Approx. 250 mm × 200 mm × 200 mm (for 1U configuration) |
| Material | Impact-resistant polymer enclosure with reinforced edges |
| Interior lining | Precision-cut anti-static foam inserts |
| Interior lining (2) | Custom slots for trays, fasteners, and tools |
Data Patterns (India) Ltd.
India · 1998 · 1 productVertically integrated Indian defence and aerospace electronics company designing and manufacturing avionics, microelectronics, RF/microwave, radar, test equipment and space systems.

Gimbal and Actuator Controller Products
BLDC motor drivers and actuator controllers for gimbal, thrust vector and control surfaces
Dcubed
Germany · 2 productsGerman manufacturer of space deployables using patented Shape Memory and Origami technologies — release actuators, solar arrays, and antenna deployables for CubeSats and microsatellites.

Nano SmartPack Release Nut (nD3SP)
The Dcubed Nano SmartPack Release Nut (nD3SP) is an ultra-flat, shape-memory alloy (SMA) based release actuator designed to secure sensitive equipment during launch and safely rele
| TRL | 9 |
| Field-resettable | in Seconds, up to 400 times |
| Short delivery time | 8-10 weeks |
| Actuation | Fully Redundant |
| Trigger | Smart SMA |

Release Nuts
A family of release nuts designed for various space applications, offering different sizes, masses, and axial load capacities.
| Dimensions (SmartPack Release Nut nD3SP) | 74x35x4 mm / 2.91x1.38x0.16 in |
| Mass (SmartPack Release Nut nD3SP) | 27 grams / 0.95 oz |
| Load (SmartPack Release Nut nD3SP) | Axial Load: 200 N / 45 lbf |
| TRL (SmartPack Release Nut nD3SP) | 9 |
| Dimensions (Nano Release Nut nD3RN) | 17x17x17 mm / 0.67x0.67x0.67 in |
DeltaV Robotics
United States · 2018 · 1 productDeltaV Robotics was founded by Niha Agarwalla and Naushad Rahman, who have experience in commercial and defense space, including flight-proven spacecraft engineering.
On-Orbit Robotic Servicing System
DeltaV Robotics' autonomous robotic arm and end-effector systems for on-orbit satellite servicing — docking, refueling, component replacement, and orbital assembly tasks.
| Technology | Autonomous robotic arm, end-effectors, AI vision and pose estimation |
| Tasks | Satellite grappling, refueling, component exchange, tethered retrieval |
| Target operations | LEO debris capture, GEO life extension, orbital assembly |
| Autonomy | Autonomous (GEO latency makes teleoperation impractical for precision tasks) |
| Programs | NASA SBIR participant, commercial LEO servicing solicitations |
DELTAV Space Technologies
Turkey · 2018 · 1 productTurkish aerospace company developing hybrid rocket propulsion, cryogenic systems, composite structures, and in-space propulsion — with a sounding rocket exceeding 200 km altitude and a hybrid propulsion system for Turkey's lunar hard landin

Composite Technologies
DELTAV Space Technologies utilizes advanced composite materials and manufacturing techniques for critical components in rocket motor bodies and nose cones, ensuring high performanc
Deployable Space Systems (DSS) — now Redwire
United States · 1 productDeployable Space Systems (DSS), now part of Redwire, develops and produces the ROSA (Roll-Out Solar Array) — the deployable solar wing powering ISS upgrades, DART, and the Gateway PPE.

Zeus Modular Payload Adapter
Zeus is a modular payload adapter built in the United States for multi-manifest, rideshare, and constellation programs, adaptable to various spacecraft sizes and interfaces.
| Dimensions (STOWED) | 1575 mm interface to PAF |
| Layout options | Option 1: Four (QTY-4) 24 inch circular ports Option 2: Six (QTY-6) 15 inch circular ports |
| Total spacecraft mass | Supports up to 1500 kg space vehicles depending on the manifest |
| Mission applications | Satellite constellation programs Rideshare programs Multi-manifest programs |
| Payload size (stowed) | 1575 mm interface to PAF |
EIE Space Technologies Srl
Italy · 1 productEIE Space Technologies Srl operates in the Space sector. The company designs and manufactures support equipment for model testing.

E-ELT – European Extremely Large Telescope
EIE GROUP is a key partner in the design and construction of the European Extremely Large Telescope (E-ELT), the world's largest optical/infrared telescope.
| Primary Mirror Diameter | 39 m |
| Telescope Height | 65 m |
| Telescope Weight (mechanisms included) | 3500 t |
| Dome Diameter | 95 m |
| Dome Height | 80 m |
ElmSpace
Germany · 1 productDeveloper of fluid-dynamic attitude control systems, gyroscopes, and air bearings for the space industry.

Fluid-Dynamic Attitude Control System (FDA)
Fluid-dynamic attitude control system for satellites — core product line providing attitude determination and control equipment for the space industry.
| Technology | Fluid-dynamic attitude control |
| Application | Satellite attitude determination and control |
Enduralock
United States · 1 productEnduralock creates a full-scale solution for satellite providers to refuel, upgrade, repair, and assemble assets directly in orbit. They engineer servicing and assembly components for satellite platforms.

OneCatch™
OneCatch™ is a deployable in-space capture mechanism providing a simple, robust, and reusable solution for a wide range of on-orbit missions, including RPOC missions.
| Actuators | 3 |
EnduroSat
Bulgaria · 2015 · 2 productsSoftware-flexible CubeSat platforms (1U–16U+), shared-satellite hosted-payload service.

12U Structure
The 12U Structure is a CubeSat frame designed to house and protect satellite components, providing a standardized form factor for space missions.
| Dimensions | 226.3 x 226.3 x 454 mm |

16U Structure
The 16U Structure is a CubeSat frame designed to house and protect satellite components, providing a standardized form factor for space missions.
| Dimensions | 226.3 x 226.3 x 366 mm |
Ensign-Bickford Aerospace & Defense (EBAD)
United States · 41 productsUS manufacturer of non-explosive actuators (TiNi FrangiBolt, pin pullers, ejectors) and energetic hold-down and release systems.

EBAD NEA® Model 2545 Pin Puller
The NEA® Model 2545 Pin Puller is a non-pyrotechnical mechanism that employs EBAD’s patented split-spool and bridge wire technology, similar to their Hold Down & Release
| Pull force at beginning of stroke | 45 lbf (200 N) |
| Pull force at end of stroke | 25 lbf (111 N) |
| Fuse wire resistance | 1.2 to 2.0 Ω @ 25°C |
| Actuation current | 4 Amps for 25 ms |
| No-fire current (continuity) | 250 mA |
EBAD NEA1120-05 Pin Puller
The EBAD NEA1120-05 Pin Puller is a non-pyrotechnic Hold Down & Release Mechanism (HDRM) designed for the spacecraft market. It employs EBAD’s patented split spool techno
| Mass | 1.66 oz [47 g] MAX |
| Number of wires | 2 TOTAL (2 PRIMARY ONLY) |
| Cable length | 30.0 in [STANDARD LENGTH] |
| Operational current | 3 Amps FOR 50 ms |
| Resistance | 0.95 to 1.6Ω @ 23°C |

EBAD TiNi frangibolt
EBAD’s frangibolt actuators are designed to operate with an EBAD supplied Titanium notched Fastener (#4 to ½” size). Various sizes are available with a nominal tensile strength ran
| Manufacturer | EBAD |
| Lead time | 24 weeks |

EBAD TiNi Micro Latch
The EBAD TiNi Micro Latch is designed for hold down and release applications, particularly for CubeSats in ‘New Space’ missions. It is characterized by its small size,
IFD100 Plug Connector
The IFD100 is a plug connector offered in shell sizes 19 and 25, with insert arrangements including 35, 4, and 20. It is designed to mate with the IFD200 receptacle. This connector
| Connector model | IFD100 |
| Style | Plug |
| Shell size | 19 |
| Insert arrangement | 35 |
| Mates with | IFD200 |
IFD200 Receptacle Connector
The IFD200 is a receptacle connector offered in shell sizes 19 and 25, with insert arrangements including 35, 4, and 20. It is designed to mate with the IFD100 plug. This connector
| Connector model | IFD200 |
| Style | Receptacle |
| Shell size | 19 |
| Insert arrangement | 35 |
| Mates with | IFD100 |
NEA 1120-05 Pin Puller
The EBAD NEA 1120-05 Pin Puller is a non-pyrotechnic Hold Down & Release Mechanism (HDRM) designed for spacecraft applications. It utilizes EBAD’s patented split spool te
| Mass | 47 g (1.66 oz) max |
| Side load | 20 lbf (88.9 N) |
| Function time | 50 ms max @ 3.0 A |
| Emitted shock | <1,000 g’s |
| Nominal actuation current | 4 Amps for 25 ms |

NEA Hold Down Release Mechanisms
EBAD’s NEA Hold Down Release Mechanisms (HDRMs) are the industry-leading non-pyrotechnic release devices for mission-critical space applications. Utilizing a split-spool desi
| Type | Non-Explosive Actuator (NEA) Hold-Down and Release Mechanisms |
| Actuation principle | Fusewire-activated split-spool release (non-pyrotechnic) |
| Shock level | Ultra-low shock |
| Variants | HDRM, pin pullers, cell bypass switches, isolation valves |
| Flight heritage | 20+ years: A2100, Spacebus, Eurostar, LS-1300, JWST |
NEA IFD100 Plug In-Flight Disconnect Connector
The NEA IFD100 Plug is part of EBAD’s Zero Separation Force (ZSF) and In-Flight Disconnect (IFD) connector series, providing reliable in-flight electrical disconnects for satellite
| Shell size | 19 |
| Insert arrangement | 35 |
| Mates with | IFD200 |
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |
NEA IFD100 Plug In-Flight Disconnect Connector (Shell Size 25)
The NEA IFD100 Plug is part of EBAD’s Zero Separation Force (ZSF) and In-Flight Disconnect (IFD) connector series, providing reliable in-flight electrical disconnects for satellite
| Shell size | 25 |
| Insert arrangement | 4, 20 |
| Mates with | IFD200 |
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |
NEA IFD200 Receptacle In-Flight Disconnect Connector
The NEA IFD200 Receptacle is part of EBAD’s Zero Separation Force (ZSF) and In-Flight Disconnect (IFD) connector series, providing reliable in-flight electrical disconnects for sat
| Shell size | 19 |
| Insert arrangement | 35 |
| Mates with | IFD100 |
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |
NEA IFD200 Receptacle In-Flight Disconnect Connector (Shell Size 25)
The NEA IFD200 Receptacle is part of EBAD’s Zero Separation Force (ZSF) and In-Flight Disconnect (IFD) connector series, providing reliable in-flight electrical disconnects for sat
| Shell size | 25 |
| Insert arrangement | 4, 20 |
| Mates with | IFD100 |
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |

NEA ZSF100 Plug Zero Separation Force Connector
The NEA ZSF100 Plug is part of EBAD’s Zero Separation Force (ZSF) and In-Flight Disconnect (IFD) connector series, providing reliable in-flight electrical disconnects for satellite
| Shell size | 21 |
| Insert arrangement | 11, 16, 35, 41 |
| Mates with | ZSF200 |
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |

NEA ZSF100/200 Zero Separation Force & In-Flight Disconnect (IFD) Electrical Interconnect
Reliable in-flight electrical disconnects for satellite and spacecraft separation, missile staging, and umbilical separation, designed to provide precision zero, positive or negati
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |
| Linear misalignment | 0.76 mm (0.03 in) min |
| Maximum angular misalignment | 20° Cone |
| Qualification temperature range | -55°C to +200°C |

NEA ZSF100P Plug Zero Separation Force Connector
The NEA ZSF100P Plug is part of EBAD’s Zero Separation Force (ZSF) and In-Flight Disconnect (IFD) connector series, providing reliable in-flight electrical disconnects for satellit
| Shell size | 17 |
| Insert arrangement | 8 DF200SS2 |
| Mates with | ZSF202S |
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |
NEA ZSF200 Receptacle Zero Separation Force Connector
The NEA ZSF200 Receptacle is part of EBAD’s Zero Separation Force (ZSF) and In-Flight Disconnect (IFD) connector series, providing reliable in-flight electrical disconnects for sat
| Shell size | 21 |
| Insert arrangement | 11, 16, 35, 41 |
| Mates with | ZSF100 |
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |
NEA ZSF202S Receptacle Zero Separation Force Connector
The NEA ZSF202S Receptacle is part of EBAD’s Zero Separation Force (ZSF) and In-Flight Disconnect (IFD) connector series, providing reliable in-flight electrical disconnects for sa
| Shell size | 25 |
| Insert arrangement | 62 |
| Mates with | ZSF100P |
| Separation force | 0 N (0 lbf) (or adjustable to customer spec) |
| Engagement force | 90 N (20 lbf) |

NEA® Model 9104 Hold Down & Release Mechanism (HDRM)
The NEA® Model 9104 is an electrically initiated, one-shot non-pyrotechnic Hold Down & Release Mechanism (HDRM) capable of supporting release loads up to 15,000 lbf (67,000 N).
| Proof load rating | 18,750 lbf (84,000 N) |
| Release load rating | 15,000 lbf (67,000 N) |
| Shock @ preload | <750 g's @ 15,000 lbf (67,000 N) |
| Fuse wire resistance | 1.2 to 2.0 Ω @ 25°C |
| Actuation current | 4 Amps for 25 ms |

TiNi ERM E1000 Ejector Release Mechanism
The EBAD TiNi™ Ejector Release Mechanism E1000 is a derivative of the TiNi™ Pin Pullers, employing a Shape Memory Alloy (SMA) wire threaded through a latch and attached to electric
| Max release load | 1,000 lbf (4,448 N) |
| Proof load | 1,400 lbf (6,230 N) |
| Max torque | 32 in-lb |
| Coupler kick off-force | 9.5 lbf |
| Max misalignment capability | +/- 5º engagement and deployment |

TiNi ERM E2000 Ejector Release Mechanism
The EBAD TiNi™ Ejector Release Mechanism E2000 is a derivative of the TiNi™ Pin Pullers, employing a Shape Memory Alloy (SMA) wire threaded through a latch and attached to electric
| Max release load | 2,000 lbf (8,900 N) |
| Proof load | 2,500 lbf (11,125 N) |
| Max torque | 70 in-lb |
| Coupler kick off-force | 8.5 lbf |
| Max misalignment capability | +/- 5º engagement and deployment |

TiNi ERM E250 Ejector Release Mechanism
The EBAD TiNi™ Ejector Release Mechanism E250 is a derivative of the TiNi™ Pin Pullers, employing a Shape Memory Alloy (SMA) wire threaded through a latch and attached to electrica
| Max release load | 250 lbf (1,112 N) |
| Proof load | 350 lbf (1,557 N) |
| Max torque | 92 in-oz |
| Coupler kick off-force | 1.5 lbf |
| Max misalignment capability | +/- 5º engagement and deployment |

TiNi ERM E4000 Ejector Release Mechanism
The EBAD TiNi™ Ejector Release Mechanism E4000 is a derivative of the TiNi™ Pin Pullers, employing a Shape Memory Alloy (SMA) wire threaded through a latch and attached to electric
| Max release load | 4,000 lbf (17,800 N) |
| Proof load | 5,000 lbf (22,400 N) |
| Max torque | 250 in-lb |
| Coupler kick off-force | 18 lbf |
| Max misalignment capability | +/- 5º engagement and deployment |

TiNi ERM E500 Ejector Release Mechanism
The EBAD TiNi™ Ejector Release Mechanism E500 is a derivative of the TiNi™ Pin Pullers, employing a Shape Memory Alloy (SMA) wire threaded through a latch and attached to electrica
| Max release load | 500 lbf (2,224 N) |
| Proof load | 700 lbf (3,114 N) |
| Max torque | 14 in-lb |
| Coupler kick off-force | 6.5 lbf |
| Max misalignment capability | +/- 5º engagement and deployment |
TiNi Flat Pack FP50 Frangibolt Actuator
The EBAD TiNi™ Frangibolt® Actuator is a simple and effective way to support and release loads. The FP50 is a specific model within this product line. The principle of operation in
| Mass | 1.17 oz (33 g) max |
| Power | 1.25 W @ .75 A |
| Operational current | .4 A to 1.5 A |
| Resistance | 3.3±.3 Ω @ 23°C |
| Max release load | 50 lbf (222.4 N) |
TiNi Frangibolt Actuator FB12
The EBAD Frangibolt® Actuator is a simple and effective non-pyrotechnic separation system for satellite applications. The FB12 model utilizes a Shape Memory Alloy (SMA) cylinder th
| Ti fastener size | 1" |
| Mass | 350 g |
| Power | 143 W @ 100 V |
| Operational voltage* | 95-105 V |
| Current draw | 1.4 A @ 100 V |

TiNi Frangibolt Actuator FC2
The EBAD Frangibolt® Actuator is a simple and effective non-pyrotechnic separation system for satellite applications. The FC2 model utilizes a Shape Memory Alloy (SMA) cylinder tha
| Ti fastener size | #8 |
| Mass | 25 g |
| Power | 25 W @ 28 V |
| Operational voltage* | 22-36 V |
| Current draw | .9 A @ 28 V |

TiNi Frangibolt Actuator FC3
The EBAD Frangibolt® Actuator is a simple and effective non-pyrotechnic separation system for satellite applications. The FC3 model utilizes a Shape Memory Alloy (SMA) cylinder tha
| Ti fastener size | #10 |
| Mass | 40 g |
| Power | 49 W @ 28 V |
| Operational voltage* | 22-36 V |
| Current draw | 1.75 A @ 28 V |

TiNi Frangibolt Actuator FC4
The EBAD Frangibolt® Actuator is a simple and effective non-pyrotechnic separation system for satellite applications. The FC4 model utilizes a Shape Memory Alloy (SMA) cylinder tha
| Ti fastener size | 1/4" |
| Mass | 55 g |
| Power | 80 W @ 28 V |
| Operational voltage* | 22-36 V |
| Current draw | 2.9 A @ 28 V |

TiNi Frangibolt Actuator FC6
The EBAD Frangibolt® Actuator is a simple and effective non-pyrotechnic separation system for satellite applications. The FC6 model utilizes a Shape Memory Alloy (SMA) cylinder tha
| Ti fastener size | 3/8" |
| Mass | 110 g |
| Power | 111 W @ 100 V |
| Operational voltage* | 95-105 V |
| Current draw | 1.1 A @ 100 V |
TiNi Frangibolt Actuator FC8
The EBAD Frangibolt® Actuator is a simple and effective non-pyrotechnic separation system for satellite applications. The FC8 model utilizes a Shape Memory Alloy (SMA) cylinder tha
| Ti fastener size | 1/2" |
| Mass | 175 g |
| Power | 112 W @ 28 V |
| Operational voltage* | 22-36 V |
| Current draw | 4 A @ 28 V |

TiNi MINI Frangibolt FD04 Actuator
EBAD’s Mini-Frangibolt® Actuators are utilized in satellite applications to provide a simple and effective non-pyro separation system between two components. With the ability to cu
| Ti fastener size | #4 |
| Mass | 10 g |
| Power | 9 W @ 7 V |
| Operational voltage | 6-8 V |
| Current draw | 1.25 A @ 7 V |

TiNi Pin Puller P10
EBAD’s TiNi Pin Pullers are utilized in satellite applications to provide a simple and effective non-pyro separation system between two components where a pull force is required. T
| Pull force | 10 lbf (44 N) |
| Side load (actuation) | 10 lbf (44.5 N) |
| Side load (non-actuation) | 100 lbf (444.8 N) |
| Mass | 1.06 oz (30 g) |
| Operating current | .4 to 1.5 A |

TiNi Pin Puller P100
EBAD’s TiNi Pin Pullers are utilized in satellite applications to provide a simple and effective non-pyro separation system between two components where a pull force is required. T
| Pull force | 100 lbf (445 N) |
| Side load (actuation) | 100 lbf (445 N) |
| Side load (non-actuation) | 490 lbf (2,180 N) |
| Mass | 5.3 oz (150 g) |
| Operating current | 2.25 A to 6.5 A |

TiNi Pin Puller P1000
EBAD’s TiNi Pin Pullers are utilized in satellite applications to provide a simple and effective non-pyro separation system between two components where a pull force is required. T
| Pull force | 1,000 lbf (4,450 N) |
| Side load (actuation) | 200 lbf (890 N) |
| Side load (non-actuation) | 600 lbf (2,670 N) |
| Mass | 12.7 oz (360 g) |
| Operating current | 2.25 A to 6.5 A |

TiNi Pin Puller P25
EBAD’s TiNi Pin Pullers are utilized in satellite applications to provide a simple and effective non-pyro separation system between two components where a pull force is required. T
| Pull force | 25 lbf (111 N) |
| Side load (actuation) | 20 lbf (89 N) |
| Side load (non-actuation) | 330 lbf (1,468 N) |
| Mass | 1.7 oz (48 g) |
| Operating current | .6 to 2 A |

TiNi Pin Puller P5
EBAD’s TiNi Pin Pullers are utilized in satellite applications to provide a simple and effective non-pyro separation system between two components where a pull force is required. T
| Pull force | 5 lbf (22 N) |
| Side load (actuation) | 7 lbf (31.1 N) |
| Side load (non-actuation) | 20 lbf (8.9 N) |
| Mass | .73 oz (18 g) |
| Operating current | .5 to 2 A |

TiNi Pin Puller P50
EBAD’s TiNi Pin Pullers are utilized in satellite applications to provide a simple and effective non-pyro separation system between two components where a pull force is required. T
| Pull force | 50 lbf (222 N) |
| Side load (actuation) | 50 lbf (222 N) |
| Side load (non-actuation) | 400 lbf (1,823 N) |
| Mass | 2.6 oz (75 g) |
| Operating current | 1.25 A to 4.5 A |

ZSF100 Plug Connector
The ZSF100 is a plug connector offered in shell sizes 21 and 25, with insert arrangements including 11, 16, 35, 41, 7, 19, 24, 61, and 62. It is designed to mate with ZSF200, ZSF20
| Connector model | ZSF100 |
| Style | Plug |
| Shell size | 21 |
| Insert arrangement | 11, 16, 35, 41 |
| Mates with | ZSF200 |

ZSF100P Plug Connector
The ZSF100P is a plug connector featuring a shell size of 17 and an 8-pin insert arrangement. It is designed to mate with the DF200SS2 receptacle. This connector offers zero separa
| Connector model | ZSF100P |
| Style | Plug |
| Shell size | 17 |
| Insert arrangement | 8 |
| Mates with | DF200SS2 |
ZSF200 Receptacle Connector
The ZSF200 is a receptacle connector featuring a shell size of 21 and insert arrangements including 11, 16, 35, and 41. It is designed to mate with the ZSF100 plug. This connector
| Connector model | ZSF200 |
| Style | Receptacle |
| Shell size | 21 |
| Insert arrangement | 11, 16, 35, 41 |
| Mates with | ZSF100 |
ZSF202S Receptacle Connector
The ZSF202S is a receptacle connector featuring a shell size of 25 and a 62-pin insert arrangement. It is designed to mate with the ZSF100P plug. This connector offers zero separat
| Connector model | ZSF202S |
| Style | Receptacle |
| Shell size | 25 |
| Insert arrangement | 62 |
| Mates with | ZSF100P |
Exolaunch
Germany · 2008 · 2 productsBerlin-based launch and deployment services company providing end-to-end rideshare missions, satellite integration, and proprietary separation hardware for small satellites.

EXOport
Multi-satellite adapter mounting a full smallsat cluster on a single 15" or 24" ESPA/SpaceX Dispenser Ring port; 8 missions flown.
| Interface ports | 15" or 24" ESPA / SpaceX Dispenser Ring |
| Compatible separators | CarboNIX 8", 15", 18.25", 24" |
| Compatible deployers | EXOpod Nova, EXOpod AIR |
| CUBESAT range | 0.25U and above |
| Microsat range | Up to 500 kg |

EXOtube
Launch vehicle-agnostic universal modular adapter for rideshare missions, accommodating CubeSats to 1000 kg microsatellites.
| Maximum satellite mass | 1000 kg |
| Compatible separation systems | CarboNIX, Quadro Arrow, Quadro Versa |
| Compatible deployers | EXOpod Nova, EXOpod AIR |
| Compatible adapters | EXOport |
| Satellite range | CubeSats (0.25U+) to 1000 kg microsatellites |
FAULHABER Drive Systems
Germany · 6 productsFAULHABER Drive Systems manufactures DC-Motors, Brushless DC-Motors, Motors with integrated Electronics, Stepper Motors, Linear Motors, Precision Gearheads, Linear Actuators, Encoders, and Drive Electronics. They also provide accessories su

B-Flat
The FAULHABER B-Flat series offers brushless DC motors with a flat design, ideal for applications requiring compact and powerful drive systems in space and other demanding environm

Brushless DC-motors with integrated Speed Controller | BXT SC
The BXT SC series offers brushless DC-motors with an integrated speed controller, providing a compact and efficient solution for various applications.
| Speed range | [min-1] |
| Rated speed | [min-1] |

BX4 IMC
Compact brushless motors with integrated Motion Controller, suitable for applications in satellites and space exploration.

FAULHABER GPT Planetary Gearheads
FAULHABER GPT planetary gearheads offer high torque, precision, and efficiency in a compact design, ideal for demanding space applications.
| Gearhead diameter | 22 ... 42 mm |
| Material | stainless steel |
| Continuous torque | 0.45 ... 18 Nm |
| Continuous input speed | up to 15,000 min-1 |
| Intermittent torque | 0.6 ... 25 Nm |

Motion Controllers for DC Micro motors
FAULHABER motion controllers are designed for precise control of DC micro motors, offering high performance and reliability for demanding applications.
| Voltage ranges - Motor | max. 30 V |
| Voltage ranges - Electronics | max. 30 V, optionally separated |
| Continuous current | 2 A |
| Peak current | 3 A |
| Motor types | DC + Encoder |

Speed Controllers
FAULHABER speed controllers are designed for DC and BLDC motors, offering precise control and high performance for various applications, including those in aerospace and aviation.
| PWM switching frequency | 96 kHz |
| Efficiency electronic | 95 % |
Froberg Aerospace
United States · 2016 · 1 productDeveloper of multimode chemical-electric propulsion systems for small satellites.
Spacecraft Mechanisms and Deployment Systems
Froberg Aerospace's precision spacecraft mechanisms, deployment actuators, and hold-down release systems for European satellites and launch vehicles.
| Products | Deployment actuators, hold-down releases, antenna pointing drives, solar array drives |
| Actuators | SMA (shape-memory alloy), paraffin — non-pyrotechnic ('green' release) |
| Pointing drives | Antenna reflector positioners, solar array drives (continuous rotation) |
| Life | 15+ year qualified for GEO orbit |
| Standards | ESA ECSS qualification |
Frond Space Systems
New Zealand · 2020 · 1 productFrond Space Systems is a New Zealand space technology company specialising in satellite deorbiting solutions, bus platforms, and subsystem components for the CubeSat and small satellite market.

Boom System
A versatile deployable boom system for spacecraft, offering lengths up to 2m (with plans for 16m) and various deployment modes, including auto-retraction.
| Deployable length (initial) | 2m |
| Environmental qualification | GEVS levels (14.1Grms) |
| Operational temperature range | -30°C to +60°C |
| Boom tip payload wiring | 12 wires embedded for power and data |
| Hdrm | Single circuit included by default (burn-wire and SMA options available) |
Gama Space
France · 1 productGama Space develops solar sail propulsion for low-cost deep space missions and Astrobrake, an autonomous drag sail for satellite deorbiting compliance.

Astrobrake
Astrobrake is an independent, passive deorbitation device for spacecraft, designed to ensure regulatory compliance and mitigate space debris without requiring power or control from
| Mass | 900 g |
| Dimensions | 0.75 U |
| Lifetime | 10 years |
GITAI
Japan · 1 productGITAI develops robotic technologies for space exploration, including solutions for satellite construction, lunar settlements, and Martian cities, with a robot currently on the ISS.

Space Robotics and In-Space Assembly
GITAI's general-purpose space robots for ISS external maintenance, lunar surface operations, and in-space manufacturing — reducing the need for costly and dangerous human spacewalk
| Robot | S2 robotic arm — force-sensing, teleoperated, general-purpose |
| Iss demo | 2021 external ISS maintenance (Nanoracks Bishop Airlock) — first private company ISS robot |
| Target markets | Space station maintenance, lunar surface construction, in-space assembly |
| Key investor | Yamaha Motor (robotics manufacturing expertise) |
| HQ | Tokyo, Japan (US subsidiary in Los Angeles) |
GomSpace
Denmark · 2007 · 6 productsGomSpace is a Danish CubeSat manufacturer producing satellite platforms, subsystems, and end-to-end mission solutions. Products include the NanoCom radio modules, NanoPower EPS, and complete 1U–12U satellite platforms. GomSpace has one of t

16U satellite structure
The NanoStruct 16U provides ample room for payloads, power, and advanced systems, enabling the development of larger and more complex missions.

Nanostruct 6U
NanoStruct 6U offers a compact, reliable, and cost-efficient structure to host your mission payloads, enabling faster access to orbit and supporting versatile applications.
| Default structure mass | 665 g |
| Available for Payload | Up to 3U |
| Material | Aluminum 7075 |
| Outside measurements (with killswitches retracted) | 340.5 x 226.3 x 100.0 mm |
| Mass | 665 g |

NanoUtil FPP Top
The NanoUtil FFP Top is a Flight Preparation Panel for nanosatellites, designed for use in the top or bottom of 1U, 2U, or 3U nano-satellites.
| Dimensions | 98.0 mm x 98.0 mm x 8.5 mm |
| Mass | 12 g |
| Operating temperature | -40…85 °C |

NanoUtil FPP Top-S
The NanoUtil FPP Top-S is a small Flight Preparation Panel designed for 1U, 2U, or 3U nano-satellites.
| Operating temperature | -40…85 °C |
| Mass | 6 g |
| Dimensions | 98.0 x 28.0 x 8.0 mm |
| Storage temperature | -40…85 °C |

NanoUtil Interstage
The NanoUtil Interstage is an interstage panel compatible with 2U and 3U structures, providing interfaces and functions for integrated satellites and supporting active deployment o
| Supply voltage | 5 V |
| Interface | USB (Mini-B), FPP connector (2.54 mm header), PicoBlade™ connectors |

NanoUtil Interstages GSSB
Interstage panels with GomSpace Sensor Bus functionality, designed to tie the external part of the satellite to the internal, and allow mounting of fine-sun sensors and antenna tie
| Dimensions | 82.5 mm x 29.0 mm x (device dependent) |
| Mass | ~11 g |
| Operating temperature | -40 °C to +85 °C |
| Supply voltage | 3.3 V |
| PCB material | Glass/polyimide |
Gran Systems
United States · 3 productsSystem integrator and manufacturer of CubeSat structures, buses, and MyPOD test/transport pods, with space environment test equipment services.

1U Cube Structure
The 1U Cube Structure is a lightweight aluminum frame designed for CubeSat missions, providing a robust housing for internal components.
| Temperature | -50°C to +120°C |
| Dimensions | Length 100 x Width 100 x Height 113.5 mm |
| Max. pc105 PCB size | 95.9 x 95.9 mm |
| Average weight | 118 g |
| Material | Aluminum T6 6061 |

3U CubeSat Structure
A 3U CubeSat structure made from Aluminum T6 6061, designed to house PC104-compatible PCBs and withstand a wide range of temperatures.
| Temperature | -50°C to +120°C |
| Dimensions | L 100 × W 100 × H 340 mm |
| Max. pc105 PCB size | 95.9 x 95.9 mm |
| Deployable dimensions | L 104 × W 104 × H 340 mm |
| Average weight | 580 g |

6U Cube Structure
The 6U Cube Structure is a lightweight aluminum frame designed for CubeSat missions, offering robust environmental characteristics and customizable mounting options.
| Temperature | -50°C to +120°C |
| Dimensions | L 100 × W 226.3 × H 366 mm |
| Deployable dimensions | L 104 × W 230.3 × H 366 mm |
| Average weight | 916 g |
| Material | Aluminum T6 6061 |
Harmonic Drive
United States · 57 productsHarmonic Drive produces high precision gears, actuators, and servo drives. They offer rotary actuators, linear actuators, integrated actuators, gear units, and component sets.

CSD-2A Component Set
The ultra-flat CSD precision gears are available in seven sizes, with ratios 50:1 to 100:1, designed for high precision applications like robotics in tight spaces.
| Rated Torque L10 | 3.7 Nm |
| Limit for Repeated Peak Torque | 12 Nm |
| Limit for Momentary Peak Torque | 24 Nm |
| Backdriving Torque | 2.5 Nm |
| Standard Accuracy | 1.5 arc min |

CSD-2UF Gear Unit
The CSD-2UF is a zero-backlash gear unit available in 6 sizes with ratios from 50:1 to 100:1, offering peak torques from 12 to 450 Nm.
| Rated Torque L10 | 3.7 Nm |
| Limit for Repeated Peak Torque | 12 Nm |
| Limit for Momentary Peak Torque | 24 Nm |
| Backdriving Torque | 2.5 Nm |
| Standard Accuracy | 1.5 arc min |

CSD-2UH Gear Unit
This housed gear is compact and ultra-flat, available in 7 sizes with ratios from 50:1 to 100:1, offering zero backlash and high load capacity.
| Reduction ratios | 30:1 to 160:1 |
| Rated Torque L10 | 3.7 Nm to 329 Nm |
| Limit for Repeated Peak Torque | 12 Nm to 686 Nm |
| Limit for Momentary Peak Torque | 24 Nm to 1,440 Nm |
| Backdriving Torque | 2.5 Nm to 67 Nm |

CSF-1U-CC Miniature Gear Units
The CSF 1U-CC mini gearheads are designed for motor mounting with an adapter plate, offering shaft or flange output and zero backlash.
| Zero backlash | Yes |
| High positioning accuracy | ± 1.5 to 10 arc-min |
| Diameter | ⌀13 mm~52 mm |
| Mass | 11.4 g~335 g |
| Tooth profile | S |

CSF-1U-CC-F Miniature Gear Units
The CSF-1U-CC-F Miniature Gear Units offer zero backlash and high positioning accuracy in a very compact package, ideal for demanding space applications.
| Zero backlash | Yes |
| High positioning accuracy | ± 1.5 to 10 arc-min |
| Diameter | ⌀21 mm~52 mm |
| Mass | 25 g~295 g |
| Tooth profile | S |

CSF-1U-F Miniature Gear Units
The CSF-1U-F Miniature Gear Unit is a compact gearhead from Harmonic Drive, featuring a flange output and shaft input, available in four sizes with reduction ratios from 30:1 to 10
| Outline Dimensions | 20 mm~51 mm |
| Reduction ratios | 30:1~100:1 |
| Peak Torque | 0.13~28 Nm |
| Mass | 35 g |

CSF-2A
The Harmonic Drive® CSF component set is compact and can be directly integrated into your machinery/equipment, available in a variety of sizes and ratios.
| Rated Torque L10 | 0.9 Nm |
| Limit for Repeated Peak Torque | 1.8 Nm |
| Limit for Momentary Peak Torque | 3.3 Nm |
| Backdriving Torque | 0.65 Nm |
| Standard Accuracy | 2 arc min |

CSF-2UH-LW Gear Unit
The CSF-2UH-LW Gear Unit is a lightweight gearhead ideal for applications where weight is a critical factor, offering exceptional accuracy and repeatability in a compact and robust
| Zero Backlash | Yes |
| Weight Reduction | 30% average lower than Standard Series |
| Peak Torque | 9 Nm to 2600 Nm |
| Reduction Ratios | 30:1 to 160:1 |
| Accuracy | High |

CSF-2UP
These new gear units have an ultra-flat configuration with high-moment stiffness, ideal for applications requiring smaller, space-saving components.

CSF-2UP Ultra Flat Gearhead
The CSF-2UP gear units are the newest models in the CSF mini-series lineup, featuring an ultra-flat configuration with high-moment stiffness.
| Ratios | 30:1 to 100:1 |
| CSF-8-30-2UP Mass | 0.2 kg |
| CSF-8-50-2UP Mass | 0.2 kg |
| CSF-8-100-2UP Mass | 0.2 kg |
| CSF-11-30-2UP Mass | 0.33 kg |

CSF-2XH Miniature Gear Units
The CSF-2XH miniature gearheads are designed to couple directly to any servomotor, offering zero backlash and high positioning accuracy in a compact package.
| Gear Ratios | 30:1 to 100:1 |
| Peak Torque | 0.5~28 Nm |
| Positioning Accuracy | ± 1.5 to 10 arc-min |
| Diameter | 22 mm~53 mm |
| Output | Flange (F) or Shaft (J) |

CSF-8-30-1U-CC-F Miniature Gear Units
This miniature gearhead features a flange output, designed for direct coupling to high-performance small servomotors.
| Series | CSF |
| Size | 8 |
| Ratio | 30 |
| Type | 1U-CC-F |
| Rated Torque L10 | 0.9 Nm |

CSF-GH Harmonic Drive® gearhead
Zero-backlash CSF-GH Harmonic Drive® gearheads are available with reduction ratios from 50:1 to 160:1, utilizing a proprietary S tooth profile for high torque and accuracy.
| Peak Torque | 18 Nm to 2,630 Nm |
| Ratios | 50:1 to 160:1 |
| Accuracy | <1 arc-min |
| Repeatability | ±4 to ±10 arc-sec |
| Available Sizes | 5 |

CSG-2A Component Set
Harmonic Drive® CSG Series gearing component sets are second generation cup-type component sets, ideal for high torque applications.
| Peak Torque | 23 Nm to 3419 Nm |
| Zero Backlash | Yes |
| High Accuracy | Yes |
| High load capacity output bearing | Yes |
| Lightweight versions also available | Yes |

CSG-2UH Zero Backlash Gear Unit
The CSG-2UH is a high torque housed component gear set combined with a precision cross roller output bearing & flange, offering a compact, robust, and easy-to-use gearhead solu
| Peak Torque | 23 Nm to 3419 Nm |
| Accuracy | <1 arc-min |
| Reduction ratios | 30:1 to 160:1 |
| Rated Torque L10 | 7 Nm to 1236 Nm |
| Limit for Repeated Peak Torque | 23 Nm to 3419 Nm |

CSG-2UH-LW Gear Unit
A lightweight, high-torque gear unit with zero backlash, ideal for applications where weight is a critical factor.
| Peak Torque | 23 Nm to 3419 Nm |
| Reduction ratios | 30:1 to 160:1 |
| Standard Accuracy | 1 arc min |
| Series | CSG |
| Model | 2UH-LW |

CSG-GH
Harmonic Drive® CSG-GH gearheads offer zero-backlash, 30% higher torque, and 42% longer life than standard models, featuring a proprietary S tooth profile and Quick Connect® coupli
| Peak Torque | 23 Nm to 3,419 Nm |
| Ratios | 50:1 to 160:1 |
| Accuracy | <1 arc-min |
| Repeatability | ±4 to ±10 arc-sec |
| Frame Sizes | 5 |

DDP Servo Drive
The DDP Servo Drive is a compact and versatile DC digital servo drive designed for precise motion control in various applications, including those requiring incremental encoder fee
| Supply Voltage (DDP-090-09) | DC24V |
| Supply Voltage (DDP-090-18, DDP-090-36) | DC48 to 90 V |
| Control Modes | Indexer, Point-to-Point, PVT, Camming, Gearing, Position, Velocity, Torque |
| Command Interface | CANopen/DeviceNet, ASCII and discrete I/O, Stepper commands, ±10 V position/velocity/torqu |
| Communications | CANopen/DeviceNet, RS-232 |
Direct Drive and Hollow Shaft Motors
Harmonic Drive offers reliable direct drive and hollow shaft motor options to support manufacturing processes in numerous industries, including robotics, medical devices, automotiv
| Positioning accuracy | 10 arc-sec |
| Repeatability | ±0.5 arc-sec |
| Resolution | 0.16 arc-sec |
| Frame sizes | 5 |

FB-2 Component Gear Set
The FB-2 Component Gear Set offers high ratio, in-line mechanical power transmissions in extremely compact configurations, making it easier to use than conventional gearing.
| Mass | 0.1 kg |
| Gear Backlash | < 3 arc min |
| Rated torque at 2000rpm (oil lubricant) | 14 Nm |
| Rated torque at 2000rpm (grease lubricant) | 18 Nm |
| Max. Repeated Peak Torque (oil lubricant) | 18 Nm |

FB-32-157-2-GR Flat Component Set
The FB-32-157-2-GR is a flat component set from Harmonic Drive, consisting of a wave generator, flexspline, circular spline, and dynamic spline, designed for precise motion control
| Rated Torque L10 | 82 Nm |
| Limit for Average Torque | 118 Nm |
| Limit for Repeated Peak Torque | 157 Nm |
| Limit for Momentary Peak Torque | 235 Nm |
| Ave. Input Speed | 2,300 rpm |

FBB Phasing Differential
FBB gear sets allow easy and direct phasing of rotating elements and are ideally suited for web presses and other machines requiring constant monitoring and adjustment while they a
| Maximum Input RPM (Oil) | 6000 |
| Maximum Input RPM (Grease) | 3500 |
| Rated Torque @1750 RPM (lb-in) | 246 - 3180 |
| Rated Torque @1750 RPM (Nm) | 28 - 359 |
| Maximum Output Torque (lb-in) | 250 - 5800 |

FD-0A Phasing Differential
The FD series is an extremely compact differential unit that allows you to fine-tune the phase and timing during operation.
| Mass(kg) 20 | 2.0 |
| Mass(kg) 25 | 2.6 |
| Mass(kg) 32 | 5.0 |
| Mass(kg) 40 | 8.3 |
| Mass(kg) 50 | 17 |

FD-2A Differential Gear
The FD series is an extremely compact differential unit that allows you to fine-tune the phase and timing during operation.
| Mass (Size 20) | 0.6 kg |
| Mass (Size 25) | 1.0 kg |
| Mass (Size 32) | 2.0 kg |
| Mass (Size 40) | 3.6 kg |
| Mass (Size 50) | 7.2 kg |

FHA-C
Super-flat hollow shaft actuators with high torque, high positioning accuracy and high torsional stiffness, ideal for various space applications.
| Peak torque | 39~820 Nm |
| Max speed | 22~96 rpm |

FHA-C LW Mini
The FHA-C Lightweight Mini is a compact, flat-profile actuator designed for applications where every gram and every millimeter matter.

FHA-Mini Actuator with Integrated Servo Drive
The FHA-C mini Series is a family of extremely compact actuators that deliver high torque with exceptional accuracy and repeatability, now available with an integrated servo drive
| Supply Voltage Range | 24VDC Nominal +7 to 28VDC |
| Output Sensing Encoder Resolution | 14bit (16384 cpr) |
| Input Sensing Encoder Resolution | 15bit (32768 cpr) |
| Safety Standard | EN60034-1:2010, EN60034-5 |
| One-way Positioning Accuracy (FHA-8C) | 150 arc-sec |

FHA-Mini Compact Hollow Shaft Servo Actuator
The FHA-C Mini Series is a family of extremely compact Actuators that deliver high torque with exceptional accuracy and repeatability, combining a high precision Harmonic Drive® ge
| Maximum Torque (FHA-14C, 100) | 28 N.m |
| Maximum Speed | 200 rpm |
| Positioning Accuracy | 90 arc-sec |
| Maximum Moment Load (FHA-14C) | 75 Nm |
| Moment Stiffness (FHA-14C) | 8 x 10^4 Nm/rad |

FLA Ultra-Flat Rotary Actuator
The FLA Ultra-Flat Rotary Actuator combines high-precision/high-performance reducers with a compact, high-output brushless DC motor, ideal for applications like AGV wheel drives an
| Gear Ratio (HP) | 8, 9 |
| Maximum Torque (HP) | 1.8 - 12.1 Nm |
| Maximum Speed (HP) | 400 - 500 rpm |
| Weight (HP) | 390 - 1,060 g |
| Gear Ratio (FB) | 50, 100 |

FR-2 Pancake Gear
The FR-2 Pancake Gear is a heavy-duty component set designed for maximum reduction ratio in minimum space, offering low backlash and simple installation.
| Gear Backlash | < 1.5 arc min |
| Series | FR |
| Mass | 0.5 kg |
| Max. Input Speed | 6000 rpm |
| Limit for Average Input Speed | 3600 rpm |

HarmonicGrease®
HarmonicGrease® is a high-quality lubrication specifically formulated to optimize the performance and extend the life of Harmonic Drive gears, reducing friction and corrosion.
| SK-1A Temperature | 0ºC to + 40ºC |
| SK-1A Size Compatibility | Size 20 and larger |
| SK-2 Temperature | 0ºC to + 40ºC |
| SK-2 Size Compatibility | Size 17 and smaller |
| SK-3 Temperature | 0ºC to + 40ºC |

Helical Rack and Pinion Gear Set
Harmonic Drive engineers and manufactures high-precision rack and pinion gears for converting rotational movement into linear motion, utilizing cutting-edge technology and extensiv
| Helix angle | 19.5283° |
| Rack heat treatment | Induction hardened and ground |
| Rack Module 2 Length | 500 mm, 1000 mm |
| Rack Module 3 Length | 500 mm, 1000 mm |
| Pinion heat treatment | Carburized and ground |

HPG Harmonic Planetary® Precision Gearbox – Right Angle
The HPG-RA Harmonic Planetary® gearhead delivers high-torque and high-accuracy in a compact Right Angle design, incorporating continuous backlash compensation for consistent low ba
| Peak Torque | 150 Nm to 2,200 Nm |
| Ratios | 5:1 to 50:1 |
| Backlash | <3 arc-min |
| Frame Sizes | 3 |
| Rated Torque L10 | 66 Nm (min) to 800 Nm (max) |

HPG Planetary Gearbox
The HPG-A Harmonic Planetary® gearhead delivers high-torque and high-accuracy in a compact package, featuring continuous backlash compensation and a large Cross Roller bearing for
| Peak Torque | 5 Nm to 3,200 Nm |
| Ratios | 3:1 to 50:1 |
| Backlash | <3 arc-min (<1 arc-min available as an option) |
| Repeatability | ±20 arc-sec |
| Available Frame Sizes | Six |

HPG-U1 Planetary Gear
The HPG-U1 Planetary Gearhead offers high performance with an input shaft for shaft couplings or belt drives, incorporating continuous backlash compensation for consistent low back
| Peak Torque | 5 Nm to 3,200 Nm |
| Ratios | 3:1 to 50:1 |
| Backlash | <3 arc-min |
| Frame Sizes | 6 |
| Max. Input Speed | 10,000 rpm |

HPGP Planetary Gearbox
The HPGP Harmonic Planetary® gearhead uses four planet gears to deliver high torque and high accuracy in a compact package, incorporating continuous backlash compensation for low b
| Peak Torque | 12 Nm to 3,940 Nm |
| Ratios | 4:1 to 45:1 |
| Backlash | <3 arc-min |
| Repeatability | ±20 arc-sec |
| Rated Torque L10 | 3.4 Nm to 1,130 Nm |

HPN-A Planetary Gearbox
The HPN Harmonic Planetary® Value Series Gearbox offers a low-cost solution with high torque, quiet performance, and long life, without compromising on quality.
| Peak torque | 9 Nm to 752 Nm |
| Ratios | 3:1 to 50:1 |
| Backlash | <5 arc-min (single stage), <7 arc-min (two stage) |
| Frame Sizes | 5 |
| Max. Input Speed | 10,000 rpm |

HPN-L Planetary Gearbox
The HPN-L Harmonic Planetary® value series gearbox offers a cost-effective solution without compromising on quality or performance, featuring helical gears for high torque, quiet o
| Peak torque | 9 Nm to 752 Nm |
| Ratios | 3:1 to 50:1 |
| Backlash (single stage) | <5 arc-min |
| Backlash (two stage) | <7 arc-min |
| Frame Sizes | 5 |
KDU Direct Drive
The KDU Series are Direct Drive Motors designed for high-precision positioning and repeatability, featuring a large hollow shaft for versatile integration.
| Maximum torque (KDU-13SB) | 7.0 Nm (62.0 In.lb) |
| Maximum torque (KDU-13WB) | 15.0 Nm (132.8 In.lb) |
| Maximum rotational speed (KDU-13SB) | 180 rpm |
| Maximum rotational speed (KDU-13WB) | 160 rpm |
| Input power supply voltage | AC100 V |

LA Precision Linear Actuator
The LA Precision Linear Actuator offers exceptional positioning accuracy and repeatability, making it ideal for demanding applications in various high-tech industries.
| Max. driving force | 49 N (5kgf) |
| Resolution | 0.0174μm |
| Stroke | 10 mm, 30 mm |
| Maximum feed speed | 0.9 mm/s |
| Repeatability | ±0.1μm/1 mm stroke |

Laser Scanning Actuator
Harmonic Drive manufactures galvanometer scanner actuators capable of scanning at high speeds with intense precision, utilizing unique mobile magnet motors and a newly developed op
| Item/model | LSA-10A-30 |
| Maximum angular runout | ±15 deg |
| Torque constant | 0.0077 N·m/A (0.0668 In.lb/A) |
| Sensor Linearity (on full scale) | ±0.06 % |
| Scale drift | 0.005 %/°C |

Phase Adjusters
Harmonic Drive's phase adjusters are high-precision phasing differential gears designed to fine-tune phase and timing during equipment operation, ideal for demanding applications i
| Torque range | 500 in-lb to 20,000 in-lb |
| Adjustment ratio | 100:1 |

Precision Component Sets
Harmonic Drive's precision component sets are core motion control mechanisms, offering zero-backlash performance and design flexibility for various applications.
| Accuracy | <1 arc-min |
| Torque (SHF-2A) | 9.0 ~ 1800 Nm |
| Torque (SHG-2A) | 23 ~ 3400 Nm |

REL Servo Drive
The REL Servo Drive offers a versatile command interface and supports various encoder types, making it suitable for a wide range of motion control applications.
| Command Interface | CANopen over EtherCAT (CoE), ASCII and discrete I/O, Stepper commands, ±10 V position/velo |
| Control Modes | Indexer, Point-to-Point, PVT, Camming, Gearing, Position, Velocity, Torque |
| Encoder Interface | 14 wire Incremental Encoder, 4 wire Incremental Encoder, Absolute Encoder |
| Communications | EtherCAT, RS-232, RS-485 (Optional) |
| I/O – Digital | 15 inputs, 6 outputs |

RH Mini Actuator
The RH Mini Series is a DC servo actuator that incorporates Harmonic Drive® precision gears, a high-performance brush DC servomotor, and an incremental encoder.
| Mass | 0.09 kg (RH-5A) |
| Mass (2) | 0.3 kg (RH-8D) |
| Mass (3) | 0.5 kg (RH-11D) |
| Mass (4) | 0.77 kg (RH-14D) |
| Maximum momentary torque (RH-5A) | 0.39 N·m |

RKF Actuator
The RKF series is a compact servo actuator combining a zero backlash Harmonic Drive® gear and an AC servo motor, designed for operation with a wide range of third-party drives.
| Mass (RKF-20A) | 2.9 kg |
| Mass (RKF-25A) | 5.0 kg |
| Mass (RKF-32A) | 9.5 kg |
| One-way Positioning accuracy | 90 arc.sec |
| Encoder type | Incremental encoder |

RSF Actuator
The RSF series servo actuator combines a high performance brushless servomotor with a high accuracy Harmonic Drive® gearhead, delivering precise, reliable motion control for high t
| Rated Output (RSF-17A, Ratio 50) | 62 W |
| Rated Output (RSF-17A, Ratio 100) | 62 W |
| Rated Torque (RSF-17A, Ratio 50) | 9.8 Nm |
| Rated Torque (RSF-17A, Ratio 100) | 20 Nm |
| Rated Rotational Speed (RSF-17A, Ratio 50) | 60 rpm |
RSF-Mini
These brushless servo actuators utilize zero backlash Harmonic Drive® precision gears with an AC servomotor, ideal for small robot joints and semiconductor/LCD manufacturing equipm
| Model | RSF-8B, RSF-11B, RSF-14B |
| Gear Ratio | 30, 50, 100 |
| Max. Torque (RSF-14B, 100) | 28 N.m (248 In.lb) |
| Maximum Speed of Rotation | 60-200 rpm |
| Max. Continuous Torque (RSF-14B, 100) | 6.0 N.m (53.1 In.lb) |
RSF-Supermini Brushless Servo Actuator
These extremely small servo actuators utilize zero backlash Harmonic Drive® precision gears, a brushless servo motor and an incremental encoder to deliver precision motion control.
| Rated Torque (RSF-3C, 30) | 0.03 Nm |
| Rated Torque (RSF-3C, 50) | 0.07 Nm |
| Rated Torque (RSF-3C, 100) | 0.11 Nm |
| Rated Torque (RSF-5B, 30) | 0.18 Nm |
| Rated Torque (RSF-5B, 50) | 0.29 Nm |

Servo Drives
Harmonic Drive provides digital servo drives for brushless (AC) and brush (DC) actuators, compatible with various communication protocols and motor OEM encoder formats.
| Power | 4 kW |

Servo Mount Gearheads
Harmonic Drive offers easy-to-connect gearheads with a range of gear ratios and torque capacities, available as planetary or harmonic gearheads.
| Planetary Gearbox backlash (standard) | < 3 arc-min |
| Planetary Gearbox backlash (optional) | <1 arc-min |
| Harmonic Drive® gearing repeatability | ±4 to ±10 arc-sec |
| HPGP Planetary Gearbox Peak Torque | 12 Nm to 3,940 Nm |
| HPG Planetary Gearbox Repeatability | ±20 arc-sec |

SHA Integrated with Servo Drive
The SHA Integrated Series offers compact actuators delivering high torque with exceptional accuracy and repeatability, featuring Harmonic Drive® gearing, a brushless servo motor, a
| Maximum torque | 68-477 Nm |
| Maximum Speed | 16-75 rpm |
| Maximum current | 9.1-25.5 A rms |
| Continuous torque | 16-126 Nm |
| Continuous speed | 15-51 rpm |

SHD-2SH Hollow Shaft Gear
Axially compact gear units featuring a large hollow input shaft and a robust cross roller bearing, allowing loads to be mounted directly without additional support bearings.
| Rated Torque L10 | 3.7 Nm |
| Limit for Repeated Peak Torque | 12 Nm |
| Limit for Momentary Peak Torque | 23 Nm |
| Backdriving Torque | 3.7 Nm |
| Standard Accuracy | 1.5 arc min |

SHD-2UH Lightweight Gear Unit
Axially compact gear units featuring a large hollow input shaft and a robust cross roller bearing, allowing loads to be mounted directly without additional support bearings.
| Accuracy | <1 arc-min (most sizes) |
| Weight reduction | 30% lower than Standard SHF Series |
| Design | 15% shorter than SHF Series |
| Backlash | Zero |
| SHD-14-50-2UH-LW Mass | 0.49 kg |

SHF-11-50-2UH Hollow Shaft Gear Unit
The SHF-11-50-2UH is a compact hollow shaft gear unit from Harmonic Drive, designed for precision motion control applications.
| Mass | 0.53 kg |
| Rated Torque L10 | 3.5 Nm |
| Limit for Average Torque | 5.5 Nm |
| Limit for Repeated Peak Torque | 8.3 Nm |
| Limit for Momentary Peak Torque | 17 Nm |

SHF-2A Component Set
The SHF-2A Component Set is a zero-backlash component gear set featuring a brim-like mounting surface and large through hole, available in 10 sizes with reduction ratios from 30:1
| Peak torque | 9 ~ 1800 N•m |
| Ratios | 30:1 ~ 160:1 |
| Series | SHF |

SHG-50-100-2UJ Gear Unit
The SHG-50-100-2UJ Gear Unit from Harmonic Drive is a high torque gear unit designed for precision motion control applications.
| Rated Torque L10 | 611 Nm |
| Limit for Average Torque | 866 Nm |
| Limit for Repeated Peak Torque | 1,274 Nm |
| Limit for Momentary Peak Torque | 2,678 Nm |
| Starting Torque | 80 Ncm |
Hemeria
France · 2 productsHEMERIA designs, produces, and supplies space systems, vehicles, and defense equipment for commercial, institutional, and scientific customers.

Harnesses
HEMERIA designs, builds, tests and integrates interconnection solutions for equipment used in commercial, defense, and scientific space applications.

Structures
HEMERIA designs, builds, tests, and integrates aluminum sandwich or monolithic CFRP structures for various space applications, including commercial, defense, and scientific mission
| Structures designed per year | 400 |
| Satellites in orbit with HEMERIA solution | 200 |
| AIT capacity for satellites | up to 500 kg class |
| Clean room area | More than 4,000 sq-m (ISO 8) |
| Maximum structure size accommodated | 4 meters x 2 meters |
HPS High Performance Space Structure Systems
1 productHPS designs, manufactures, and integrates mechanical/thermal space subsystems, including antennas, deployable structures, thermal insulation, and equipment for nanosatellites.

LEA Large Deployable Reflector Subsystems
HPS, as LDRS-Prime, leads a European consortium (WeLEA, with LSS, Beyond Gravity Germany, and von Hoerner & Sulger) delivering complete large deployable reflector antenna subsy
| Consortium role | LDRS-Prime (WeLEA consortium) |
| Subsystem scope | Reflector, boom, hinges, hold-down/release, thermal hardware, deployment electronics |
| Applications | HYDROTERRA, CIMR/ROSE-L missions |
ISISPACE Group
Netherlands · 2006 · 2 productsCubeSat deployers, antennas, EPS and small-satellite systems.

12-Unit cubesat structure
The ISIS 12-Unit CubeSat structure is developed as a generic, modular satellite structure based upon the CubeSat standard. The design created by ISIS allows for multiple mounting…
| Manufacturer | ISISPACE |
| Lead time | 8-12 weeks |

16-Unit cubesat structure
The ISIS 16-Unit CubeSat structure is developed as a generic, modular satellite structure based upon the CubeSat standard. The design created by ISIS allows for multiple mounting…
| Manufacturer | ISISPACE |
Kairo Space
South Korea · 1 productSouth Korean nanosatellite manufacturer offering CubeSat platforms, optical imagers, star trackers, solar panels, EPS, structures, and deployers for the commercial small satellite market.

KSCS CubeSat Structure
Aluminum CubeSat structural frames in standard 1U–8U form factors for nanosatellite missions.
| Material | Aerospace-grade aluminum alloy |
| Form factors | 1U, 2U, 3U, 6U, 8U CubeSat |
| Standard | CDS-compatible |
| Deployer compatibility | P-POD, NRCSD, J-SSOD |
Kall Morris Inc
United States · 2014 · 1 productKall Morris Inc provides in-space logistics, scavenging, and long-haul transport solutions, developing spacecraft and systems for satellite mobility and orbital debris management.

Asteria Adhesive Attachment Technology
Omnidirectional gecko adhesion technology enabling permanent payload attachment to unprepared resident space objects — no continuous power required, for ISAM, deorbit, and life ext
| Adhesion type | Omnidirectional gecko adhesion |
| Power requirement | None — passive persistent attachment |
| Applications | ISAM, deorbit, life extension, tracking, defensive attachment |
| Surface compatibility | Wide range of materials and surface types |
| Dimensions | ~4" to ~12" diameter |
Kayser Space
Italy · 1986 · 1 productKayser Space designs, manufactures, integrates, and tests hardware and platforms for space programs, supporting over 100 missions and microgravity research.

Lighting Vision System
The Kayser Lighting Vision System provides stable and reliable illumination for in-orbit servicing, robotic operations, and inspection activities in the harsh space environment.
KOSMOLAB Launch Services
Russia · 2018 · 1 productCubeSat & small-satellite rideshare brokerage — integration, paperwork, launch insurance on PSLV, Falcon 9 Transporter, Ariane 6 and Soyuz.

Electric Lock
The Electric Lock is a mechanism designed for the release of actuating mechanisms in space-rocket hardware, offering custom modifications based on specific requirements.
| Dimensions (L×W×H) | 48.7 × 37.4 × 22.4 mm |
| Mass | ≤ 0.1 kg |
| Armature stroke | ≥ 4.5 mm |
| Pull force | 0.45 ± 0.05 kg |
| Operating temperature | -60°C to +60°C |
KSF Space Foundation
United States · 1 productUSA non-profit democratizing access to space technology by offering affordable CubeSat and nanosatellite hardware, suborbital launch services, near-space missions, and professional space engineering education.

CubeSat Structure (1U / 2U / 3U)
Flight-certified 1U/2U/3U CubeSat structures in aerospace-grade DMLS aluminum or PA11 polymer, validated to NASA-GSFC-STD-7000 (GEVS).
| Available sizes | 1U, 2U, 3U |
| Metal material | AlSi10Mg (Aerospace-grade Aluminium) |
| Metal process | DMLS (Direct Metal Laser Sintering) |
| Metal finish | Shot Peened |
| Polymer material | PA11 (bio-sourced nylon) |
L.Garde Inc
1971 · 1 productL.Garde designs, develops, and manufactures inflatable and deployable structures for space and terrestrial applications, including solar sails and advanced observation structures.

Deployable Space Structures (General)
L.Garde develops and tests deployable space structures, including large radar arrays and lightweight trusses with high compaction ratios, enabling advanced observation capabilities
| Isat array length | 300 meters |
| Fairing compatibility | Delta IV |
| Deployment mechanism | Concentrated strain hinges (high compaction ratio) |
| Target platforms | ESPA-class satellites |
Lamb Space Tec
Poland · 1 productPolish manufacturer of small satellites, CubeSat components, and subsystems for Earth observation and communications missions.

PEEK CubeSat Structures
Injection-molded CubeSat structures made from the high-performance polymer PEEK, offered as a lighter, more cost-effective and more sustainable alternative to conventional aluminum
| Stroke | Max. 4.5 mm |
| Force range | 4 N to 15 N |
| Max duty cycle | 90 min without external control; >240 h with external control unit |
| Design life | >500,000 cycles |
| Operating temperature | -20°C to +70°C (extendable) |
Large Space Structures GmbH
2012 · 1 productLarge Space Structures GmbH designs and manufactures large deployable reflector technologies for space applications, including LDRs and deployable antennas.

FlexRS® Category I
FlexRS® Category I are very thin and flexible shell structures, also known as Shell Membranes, designed for use as reflecting surfaces in space applications.
| Applicable frequencies | up to Ka-band |
materion
United States · 1921 · 1 productMaterion designs and manufactures advanced materials, including specialty alloys, chemicals, metals, beryllium composites, and optical coatings, for various industries including aerospace and defense.

Beryllium Optical and Structural Components
Materion's space-grade beryllium mirrors, optical benches, and structural components used in space telescopes, Earth observation sensors, and infrared instruments.
| Key material | Beryllium (density 1.85 g/cm³, modulus 287 GPa) |
| Products | Mirror blanks, optical benches, scan mirrors, structural components |
| Notable programs | James Webb Space Telescope primary mirror segments (all 18), GOES weather satellite scan m |
| Key properties | Ultra-low density, 6× stiffer than Al, excellent cryogenic stability |
| Jwst contribution | Manufactured and polished all 18 hexagonal primary mirror segments |
MDA Space
Canada · 1969 · 1 productMDA Space designs and manufactures robotics, satellite systems, and provides geointelligence services for the global defense and space industry.

Canadarm3 / Space Robotics Systems
MDA Space's Canadarm3 autonomous robotics system for NASA's Lunar Gateway, and heritage space robotics (Canadarm, Canadarm2, SPDM Dextre for ISS).
| Systems | Canadarm (Shuttle, retired), Canadarm2 (ISS), Canadarm3 (Lunar Gateway) |
| Canadarm3 feature | Autonomous operation during communication blackouts |
| Canadarm3 destination | NASA Lunar Gateway |
| Other products | Satellite antennas, RADARSAT radar satellites |
| Country | Canada (Brampton, Ontario HQ) |
Media Lario
Italy · 1 productMedia Lario produces optical components and systems for space telescopes, satellite earth observation systems, and laser optical communications systems. Their products include optical systems, optical components, and mirrored panels.

Mirrored Panels
Light-weight metallic panels designed for large segmented surface coverage, offering high shape accuracy and extended lifetime in harsh environments.
| Weight per area | 15 kg/m2 |
| Shape accuracy | better than 10 µm |
| Lifetime | 20 years |
Memetis
3 productsMemetis GmbH designs and manufactures ultracompact microvalves and highly integrated microfluidic systems for space, life science, and medical technology applications.

Custom SMA Actuators
Customizable shape memory alloy thin-foil actuators for in-space automation instruments — linear, spiral, bending, and antagonistic-linear configurations, delivering 2-5x the power
| Actuator types | Linear, Spiral, Bending, Antagonistic Linear |
| Material | Thin-foil shape memory alloy (SMA) |
| Power density | Matches conventional actuators 2-5x larger |
| Customization | Travel distance, force, and dimensions customizable |

memetis Microvalves
Ultra-compact microvalves and highly integrated microfluidic systems based on patented shape-memory-alloy actuator technology, designed for space-, life-science-, and medical-techn
| Switching cycles (fatigue-free materials) | Over 10 million |
| Customizable parameters | Pressure range, orifice, flow range, materials, housing, electronic interface |

memetis Microvalves & Microfluidic Systems
Ultra-compact microvalves and highly integrated microfluidic systems based on patented shape-memory-alloy actuator technology, designed for extreme miniaturization and low power co
| Width | 5 mm |
| Internal volume | < 6.5 µl |
| Switching cycles | Up to 10 million |
| Classic variant pressure range | 0 to 3 bar |
| Negative pressure variant range | -0.7 to 2 bar |
Micromotion GmbH
2001 · 3 productsMicromotion GmbH designs and manufactures high-precision micro drive technology, including micro drives and micro gearboxes, for various applications including space technology.

BryleeDrive Multi-Axis Micro-Drive
Combined linear-rotary multi-axis micro-drive for applications requiring simultaneous motion in more than one degree of freedom — space-rated construction.
| Motion type | Combined linear and rotary (multi-axis) |
| Environments | UHV, extreme temperature, radiation tolerant |

MaalonDrive Rotary Micro-Positioning Drive
Backlash-free rotary micro-actuator based on Harmonic Drive strain-wave gearing — arc-second repeatability, UHV and radiation-tolerant variants for space pointing mechanisms.
| Sizes | 6 mm, 8 mm, 10 mm |
| Backlash | None (strain-wave gearing) |
| Repeatability | Arc-second range |
| Environments | UHV, extreme temperature, radiation tolerant |
| Variants | Hollow shaft, ToolFit, HighAcc |

RasuunDrive Linear Spindle Drive
Linear micro-actuator with spindle drive mechanism for precision linear positioning in compact space-rated assemblies — travel distance of 3 mm or more.
| Drive type | Linear spindle drive |
| Travel distance | ≥ 3 mm |
| Environments | UHV, extreme temperature, radiation tolerant |
MinoSpace
China · 2017 · 2 productsChinese commercial satellite manufacturer building Earth observation, communications, and remote sensing satellites, plus payloads, components, and ground terminal systems.

10m-diameter flat-panel SAR antenna deployment mechanism
This product is a deployment mechanism designed for a 10m-diameter flat-panel Synthetic Aperture Radar (SAR) antenna, utilizing a passive spiral spring and a proprietary damper for
| Deployment drive | Passive spiral spring |
| Damper | Company's self-developed |
| Antenna diameter | 10m |
| Antenna type | Flat-panel SAR antenna |
| Post-deployment frequency | No less than 2 Hz |

Damper
A fully mechanical damper designed for controlled slow deployment of passive mechanisms in space applications.
MMA Design
2 productsMMA Design manufactures deployable solutions for space and terrestrial missions, including de-orbit systems and solar arrays, and is headquartered in Broomfield, Colorado.

Deployable Tape Truss Boom
Composite tape truss boom achieving expansion ratios up to 100:1 with minimum stow volumes down to 1U — building block for antennas, solar arrays, and deployable instruments.
| Expansion ratio | Up to 100:1 |
| Minimum stow volume | Down to 1U form factor |
| Underlying technology | NASA SHEARLESS boom / Bi-CTM (exclusively licensed) |
| Customization | Custom lengths via bay addition/removal |

Stand-Off Mechanism (SOM)
Flight-proven passive deployable stand-off structure using folded tape springs and a Frangibolt release mechanism — deploys to approximately 8 inches height.
| Deployed height | ~8 inches |
| Release mechanism | Frangibolt assembly |
| Energy source | Folded tape springs (passive) |
| Flight heritage | Confirmed |
Moog Space Defense Group
United States · 1951 · 13 productsPrecision motion control and propulsion systems provider for space and defense applications.

Actuators and Servo Actuators
Moog offers a comprehensive range of actuation products and technologies, transforming input signals into motion for various mechanical systems.

Linear Actuators
Moog's linear actuators translate rotary motion to linear motion, offering high performance DC motors coupled to high efficiency gearing for precise control in various applications
| Actuator Model | 981* |
| Size in (mm) | 2.50 x 4.05 x 14.00 (63.5 x 102.9 x 355.6) |
| Force lbs | 10 Rated 30 Stall |
| Stroke in | ±.65 |
| Weight lbs | 4.75 |

Model 220 Rotary Actuator
The Model 220 Rotary Servo Actuator is a versatile, high-performance electromechanical actuator designed for aerospace and unmanned airborne platforms, offering multiple communicat
| Operating Voltage | 18 to 32 VDC |
| Operating Temperature Range | -40° to +71° C |
| Operating Altitude Range | Up to 50,000 ft |
| Weight | 9 - 16 oz (depends on the configuration) |
| Life | 7,500 hrs |

Model 863 Rotary Actuator
The Model 863 is a high-performance rotary servo electromechanical actuator designed for flight control, throttle control, and other utility functions in UAV and aerospace programs
| Operating Voltage | 18 to 32 VDC |
| Operating Temperature Range | -40° to +71° C |
| Operating Altitude Range | Up to 50,000 ft |
| Mechanical Stroke | ±51.5° |
| Electrical Stroke | ±45.0° - electronically limited |

Model 905 Rotary Actuator
The Model 905 Rotary Servo Actuator is designed to position the control surfaces of the AQM-37D target drone and operates under extreme environmental conditions.
| Size | 2.3 x 4.9 x 5.4 inches |
| Load Torque (Rated) | 150 in-lbs |
| Load Torque (Peak) | 300 in-lbs |
| Stroke | ±33° |
| Weight | 3 lbs |

Model 935 Rotary Actuator
The Model 935 is a high-performance rotary servo actuator available with digital and analog communications interfaces, offering customization for angular excursion and flexible int
| Operating Voltage | 21 to 32 VDC |
| Operating Temperature Range | -40° to +71° C |
| Operating Altitude Range | -1,500 to +65,000 ft |
| Weight | 3.7 - 3.9 lbm max |

Model 965 Rotary Actuator
The Model 965 is a high-torque rotary servo electromechanical actuator that integrates position loop servo control electronics with a digital communications interface, providing an
| Operating Voltage | 21 to 32 VDC |
| Operating Temperature Range | -40° to +71° C |
| Operating Altitude Range | 11,500 to 38,000 ft |
| Weight | 11.5 lb max |
| Mechanical Stroke | ±105 ±2° non jamming stops |

Model 971 Rotary Actuator
The Moog Model 971 Rotary Servo Actuator is a military-qualified, brushless, stepper motor designed for limited rotation trim actuation in military helicopters.
| Size | 3.0 x 3.48 x 6.56 inches |
| Weight | 3.2 lbs Actuator Only |
| Power | 28 VDC |
| Holding torque | 200 in-lbs |
| Command | four phase stepper motor control from an external amplifier |

Model 974 Linear Actuator
The Model 974 linear servo actuator is designed for use in tilt rotor unmanned aerial vehicles to position nacelles during flight conversion modes, operating reliably under extreme
| Size | 3.88 x 4.75 x 14.75 inches |
| Force | 1,500 lbs |
| Rated Stroke | 7.25 in |
| Weight | 8.1 lbs |
| Power | 28 VDC |

Multi-Purpose Actuators and Servoactuators
Moog designs, develops, qualifies, and manufactures rotary and linear actuators and servoactuators for a variety of high-performance military and commercial applications.

Precision Missile Actuation Systems
Moog's Fin Control Actuation Systems (FCAS) precisely position missile control surfaces in response to steering commands from the flight computer, offering highly integrated to mod

Rotary Actuators
Moog's rotary actuators utilize brush and brushless type DC motors with neodymium and rare earth magnets, designed with separate or imbedded analog or digital amplifiers, spur gear
| Load Torque | 25 to 2,500 in-lb |
| Operating Voltage | 28 vdc |

Space Mechanisms (SADA, Gimbals, Rotary Actuators)
Moog's space mechanisms portfolio: Solar Array Drive Assemblies with 40+ years heritage, dual-axis thruster gimbals for EP systems, zero-backlash rotary actuators, and biaxial poin
| Sada — type 3/5 | Single-axis solar array drive; 40+ year heritage |
| Sada — small satellite sade | 0.8 kg; 22–34 VDC; RS-422; 88.9×101.6×48.3 mm; 50 kRad TID |
| Thruster gimbal (Model T) | Dual-axis EP thruster pointing; GEO orbit-raise and station-keeping |
| Type 55 biaxial gimbal | Dual-axis antenna/instrument pointing; output bearings carry structural loads |
| Rotary actuator type 3 | 38,400 steps/rev; 160:1 harmonic drive; 350 lb-in output torque; 4.2 lb; 14 W |
Motiv Space Systems
United States · 2014 · 5 productsMotiv Space Systems designs and builds space robotics, motor controllers, and mechanisms, including the robotic arm on NASA's Mars 2020 Perseverance rover.

CADRE (Cooperative Autonomous Distributed Robotic Exploration)
CADRE is a project developing motion control, mobility, chassis, and mechanism systems for a trio of autonomous lunar rovers, their deployer, and a base station for a NASA JPL miss
| Client | NASA Jet Propulsion Laboratory |
| Status | In Progress |
| Schedule for launch | 2024 |
| Mass | 5.6 kg |
| Payload Volume | 185 mm x 205 mm x 32 mm |

Custom Mechanisms (Mastcam-Z, SOMS Filter Wheel, Mastcam-Z Filter Wheel)
Motiv Space Systems engineers and builds custom mechanisms for space applications, including imaging systems and filter wheels for planetary rovers and Earth-orbiting platforms.
| Mastcam-z key capabilities | High-Definition Video |
| Mastcam-z key capabilities (2) | 3D Images |
| Mastcam-z key capabilities (3) | Panoramic Color Imaging |
| Mastcam-z key capabilities (4) | 28-100 mm Zoom Range |
| Mastcam-z key capabilities (5) | Ability to Resolve Features 1 mm Across at a Distance of 100-Meters |

Mars 2020 Perseverance Rover’s Primary Robotic Arm
A seven-foot long, five-DOF robotic arm designed for the Mars 2020 Perseverance rover, carrying critical science instruments for Martian exploration.
| Payload | 45 kg (Earth gravity) |
| Kinematics | 5-DOF |
| Reach | 2.1 meters |
| Environment | -135°C; Martian Dust and Radiation Hardened |
| Accuracy | <1 millimeter |

ModuLink
ModuLink is a scalable, modular, space-rated robotic system designed to enhance the capabilities and on-orbit resiliency of spacecraft through various servicing operations.

xLink™ System
The xLink™ System is a modular, scalable, and flexible robotic system designed for space applications, offering advanced robotics capabilities at competitive costs and lead times.
| Modularity | Building block approach for customization |
| Scalability | 1 meter, 3 meters; 4-DOF, 7-DOF |
| Flexibility | Component solutions to whole systems |
| Industry leading | Dexterous space robotic systems at industry leading cost and lead times |
| Flight heritage | Developed by the same team that built the robotic arm for NASA/JPL’s Mars 2020 Perseveranc |
MT Aerospace
Germany · 1995 · 3 productsGerman aerospace components manufacturer producing satellite tanks, CFRP structures, and antenna dishes for European satellite programs.

Ceramic Matrix Composite (CMC) Space Structures
MT Aerospace AG is a German manufacturer of high-performance aerospace structures based in Augsburg. The company specializes in carbon/silicon carbide (C/SiC) ceramic matrix compos

Liquid hydrogen tank
MT Aerospace offers liquid hydrogen tanks, leveraging over 50 years of experience in lightweight construction and component optimization with composite materials.

Tanks in Space
MT Aerospace has a long heritage in the development and production of tanks for various space applications, including propulsion systems and cryogenic storage.
NanoAvionics
Lithuania · 2014 · 1 productPre-integrated nanosatellite buses (3U–16U+ MP42), green chemical propulsion, mission integration.

CubeSat Structural Frame
Modular 7075-T7351 aluminum CubeSat structural frames for 6U–16U satellites, PC-104 compatible, hard-anodized, NASA GEVS 7000 compliant.
| Material | 7075-T7351 aluminum alloy |
| Finish | Hard-anodized black or natural (CubeSat standard) |
| Magnetic properties | Non-magnetic |
| Standards | CubeSat Design Specification, PC/104 stack standard |
| Shock & vibration qualification | NASA GEVS 7000 |
NazarX
Uzbekistan · 2019 · 1 productUzbekistan's first private aerospace engineering research and development center, building rocket prototypes, modular satellite platforms, and running national space-education programs.
Modular Magnetic-Connector Satellite Platform
Snap-together CubeSat module platform using magnetic connectors for rapid build, upgrade, and repair.
| Maintenance time reduction | several days to several hours |
Nimesis Technology
2008 · 2 productsNimesis Technology designs and manufactures space actuators and mechanisms using shape memory alloys for satellites, launchers, and other space applications.

HECTOR — SMA Rotary Actuator for Structural Deployment
Large-angle (90-180 deg) SMA rotary actuator for deploying booms, panels, and articulated structures on satellites and rovers — shock-free, high torque. TRL 7.
| Technology | Shape memory alloy (SMA) rotary actuator |
| TRL | 7 |
| Angular range | 90-180 degrees |
| Actuation | Electrically triggered, shock-free |
| Applications | Satellite and rover boom deployment, solar panel hinges, antennas |

SATLATCH — Rotary Deployment and Latching Mechanism
Compact SMA rotary deployment and latching mechanism for satellites — progressive shock-free deployment in 4–100 seconds, auto-resettable, operates -120°C to +120°C, vibration-qual
| Technology | CuAlNi shape memory alloy rotary mechanism |
| TRL | 8 |
| Mass | < 60 g |
| Dimensions | 40 mm wide × 8.6 mm thick |
| Deployment torque | 0.1 N·m |
Northrop Grumman Space Systems
United States · 1939 · 1 productMinotaur family, Pegasus XL, Antares (legacy); MLV co-development with Firefly.

Common Space Vehicle Mechanisms
Northrop Grumman's Common Space Vehicle Mechanisms are modular actuators designed for stowing and articulating spacecraft payloads and solar arrays, with a focus on long-life, low
| Flight heritage | 40+ years, 100% mission success, over 50 missions |
| Deployment actuators TRL | 9 |
| Solar array drive assembly TRL | 9 |
| Modular slip ring configurations | 20 or 30 ring modules |
| Modular slip ring maximum modules | Up to four modules |
NPC Spacemind
2013 · 9 productsNPC Spacemind designs and manufactures CubeSat separation systems, deployers, and subsystems, including deorbiting systems, for nanosatellites and CubeSats.

SM CubeSat Structures
Modular CubeSat structure family from 1U to 16U with configurable board stacks and deployment switches.
| Sm01 dimensions (w/o kill switches) | 113.5 x 100.0 x 100.0 mm, 1U, up to 6 deployment switches |
| Sm02 dimensions (w/o kill switches) | 227.0 x 100.0 x 100.0 mm, 2U, up to 8 deployment switches |
| Sm03 dimensions (w/o kill switches) | 340.5 x 100.0 x 100.0 mm, 3U, up to 8 deployment switches |
| Sm04 dimensions (w/o kill switches) | 454.0 x 100.0 x 100.0 mm, 4U, up to 8 deployment switches |
| Sm06 dimensions (w/o kill switches) | 340.5 x 226.3 x 100.0 mm, 6U, up to 8 deployment switches |

SM01
The SM01 is a 1U CubeSat structure designed for small satellite missions, featuring configurable board stacks and compatibility with various solar panels.
| Structure size | 1U CubeSat |
| Deployment switches | Until 6 |
| Measures (without KS) | 113.5 x 100.00 x 100.0 mm |
| Compatibility | SPM Solar Panels and multiple vendor panels |
| Board compatibility | PC104 Compatibility / PC104 PLUS Compatibility |

SM02
The SM02 is a 2U CubeSat structure designed for small satellite missions, featuring configurable board stacks, multiple deployment switches, and compatibility with PC104/PC104 PLUS
| Form factor | 2U Cubesat Structure |
| Deployment switches | Until 8 |
| Board stacks | Configurable |
| Measures (without KS) | 227.0 x 100.0 x 100.0 mm |
| PCB stack assembly | Independent from the structure |

SM03
The SM03 is a 3U CubeSat structure designed for small satellite missions, offering configurable board stacks and compatibility with various solar panels.
| Structure | 3U CubeSat Structure |
| Deployment switches | Until 8 |
| Board stacks | Configurable |
| Stack assembly | Horizontal and vertical |
| Measures (without KS) | 340.5 x 100.0 x 100.0 mm |

SM04
The SM04 is a 4U CubeSat structure designed for small satellite missions, featuring configurable board stacks and compatibility with PC104/PC104 PLUS standards.
| CUBESAT structure | 4U |
| Deployment switches | Until 8 |
| Board stacks | Configurable |
| Stack assembly | Horizontal and vertical |
| Measures (without KS) | 454 x 100.0 x 100.0 mm |

SM06
The SM06 is a 6U CubeSat structure designed for small satellite missions, featuring configurable board stacks and compatibility with various solar panels.
| CUBESAT structure | 6U |
| Deployment switches | Until 8 |
| Board stacks | Configurable |
| Stack assembly | Horizontal and vertical |
| Measures (without KS) | 340.5 x 226.3 x 100.0 mm |

SM08
The SM08 is an 8U CubeSat structure designed for small satellite missions, featuring configurable board stacks and compatibility with various solar panels.
| CUBESAT structure | 8U |
| Deployment switches | Until 8 |
| Board stacks | Configurable |
| Stack assembly | Horizontal and vertical |
| Measures (without KS) | 454.0 x 226.3 x 100.0 mm |

SM12
The SM12 is a 12U CubeSat structure designed for small satellite missions, offering configurable board stacks and compatibility with various solar panels.
| CUBESAT structure | 12U |
| Deployment switches | Until 8 |
| Board stacks | Configurable |
| Stack assembly | Horizontal and vertical |
| Measures (without KS) | 340.5 x 226.3 x 226.3 mm |

SM16
The SM16 is a 16U CubeSat structure designed for satellite integration, featuring configurable board stacks, PC104/PC104 PLUS compatibility, and options for various deployment swit
| CUBESAT structure size | 16U |
| Deployment switches | Until 8 |
| Board stacks | Configurable |
| Stack assembly | Horizontal and vertical |
| Measures (without KS) | 454.0 x 226.3 x 226.3 mm |
Opterus Research and Development
United States · 2015 · 2 productsU.S. manufacturer of deployable spacecraft structures and subsystems - booms, solar arrays and RF antennas - built on proprietary high-strain composite and origami-inspired technology.

Collapsible Tubular Mast (CTM)
The Collapsible Tubular Mast (CTM) is a precise, patent-pending boom architecture featuring a fully enclosed lenticular cross-section for greater compaction, strength, and stiffnes
| Diameter | 50-600 mm |

Living Hinge Boom
The Living Hinge Boom (LHB) is a deployable boom featuring a fully closed circular cross-section, designed for compact packaging and improved strength and stiffness.
Orbital Composites
United States · 2014 · 2 productsRobotic additive manufacturing company producing high-performance composite parts for aerospace, defense and space applications at scale.

Orbital S Multi-Robot 3D Printer
Flagship multi-robot, multi-material 3D printing platform for tooling-free composite part production.

OrbShield™
OrbShield is a single-panel solution providing radiation, thermal, and debris protection for space systems, enabling the use of COTS electronics in harsh space environments.
| Standard size | 1U |
| Custom sizes | available upon request |
Orbital Matter
Poland · 2022 · 1 productIn-space manufacturing company building 3D-printing hardware that constructs large structural booms and infrastructure directly in orbit.

Printer Assisted Deployment System (PADS)
PADS is a plug-and-play in-orbit manufacturing unit that produces rigid, continuous structural booms from 10 to over 100 meters for satellite deployables like solar arrays, radiato
| Boom length | 10 meters to over 100 meters |
| Boom diameter | Adjustable between 38 mm and 90 mm |
| Power draw during deployment | Less than a standard light bulb |
| Flight heritage | Flight qualification tests passed, launching on multiple missions in 2026 with ESA and Tha |
Orbotic Systems
United States · 1 productOrbotic Systems designs spacecraft protection, control, and orbital lifecycle management technologies, including drag-based deorbit devices, onboard threat-detection systems, and non-cooperative object capture solutions for commercial, civi

RIDDANCE
RIDDANCE is a dual-net capture system designed to detumble and secure non-cooperative objects in orbit, enabling controlled capture operations for debris remediation and on-orbit s
PacSci EMC
United States · 1975 · 2 productsPacSci EMC designs and manufactures mission-critical pyrotechnic and energetic material devices and integrated systems for aerospace, defense, energy and space applications.

Detonators
Compact detonator product line with exceptional energetic material design for space launch vehicles to deep underground energy systems.
| Design | Wide range of compact designs with extreme temperature capability |
| Initiation options | Multiple initiating stimulus options |
| Performance | Proven performance in extreme environments |
| Compliance | Meets industry and military standards |
| Engineering | Advanced analytical lab design, chemist-developed formulations |

Explosive Bolts
Explosive bolts are pyrotechnic fasteners designed for rapid structural separation in applications such as missiles, launch vehicles, and spacecraft, available in various sizes and
| Input stimulus, typical | 3.5 amp (when electrically initiated) |
| Input stimulus, typical (2) | TLX or SMDC input |
| Input stimulus, typical (3) | 4.5 AMP/4.1 millisecond |
| Tensile strength | Up to 550,000 lbf |
| Operating temperature | Designs as low as -65 °F and up to +270 °F |
Perigee Aerospace
South Korea · 2018 · 1 productSouth Korean small launch vehicle company developing the liquid-methane Blue Whale rocket family and in-house propulsion systems.

CFRP Engineering
Perigee Aerospace offers lightweight and durable carbon composite structures, from materials and design to production, enabling higher payloads and lower thermal loss for launch ve
| Diameter standard 1 | 0.76 m |
| Diameter standard 2 | 1.6 m |
| Diameter customizable | 0.3 to 2.0 m |
| Length standard 1 | 1.8 m |
| Length standard 2 | 1.8 m |
Phytron GmbH
Germany · 3 productsPhytron GmbH manufactures stepper motors, end stages, controllers, mechanics, and equipment. They develop drive solutions for various applications, including those requiring high precision and reliability under extreme conditions.

phySPACE Schrittmotoren für Weltraumanwendungen
Phytron's space-qualified stepper motors are designed for ultra-high vacuum applications, offering high precision, robustness, and minimal magnetic radiation.

phySPACE Stepper Motors for NASA’s CLPS Initiative
Phytron's specially developed phySPACE stepper motors are flying to the Moon as part of NASA's CLPS Initiative, integrated into a high-precision instrument from the University of B

Resolver für VSS Schrittmotoren der Baugrößen 25 bis 126
Phytron offers resolvers for VSS stepper motors in sizes 25 to 126, suitable for various applications including space.
PIAP Space
Poland · 2020 · 2 productsPolish robotics and space technology company developing robotic systems, space mechanisms, and rover technologies for planetary exploration and satellite servicing missions.

PIAP Space Robotic Manipulator Systems
Polish robotics company developing robotic manipulator arms and mechanisms for in-space servicing and satellite assembly missions.
| Products | Robotic manipulator arms and mechanisms |
| Applications | In-space servicing, satellite assembly, debris removal |
| Country | Poland |

TITAN — 7-DOF Orbital Robotic Arm
PIAP Space's TITAN is a 7-DOF, 2-metre reach orbital robotic arm developed under ESA contract to TRL 6: 0.5 mm positioning accuracy, redundant power/data per joint, configurable en
| Degrees of freedom | 7 |
| Reach | 2 m |
| Positioning accuracy | 0.5 mm |
| Orientation accuracy | 0.1° |
| Joint redundancy | Independent power, data bus, and thermal control per joint |
Plan-S (Connecta)
Turkey · 2021 · 1 productPlan-S designs, manufactures, launches, and operates satellite systems for IoT connectivity (Connecta) and Earth observation data analytics (Observa), with 21 satellites launched.

Plan-S (Connecta) Satellite Deployable Structures
Turkish company developing deployable structures and mechanisms for CubeSats and small satellites, including solar panel deployment systems.
| Products | Deployable structures, solar panel and antenna deployment mechanisms |
| Applications | CubeSats, small satellites |
| Country | Turkey |
Princeton Satellite Systems
United States · 1992 · 1 productAdvanced aerospace and energy technology company specializing in spacecraft GN&C software toolboxes, satellite design tools, fusion propulsion research (Starfire/DFD), CubeSat hardware, and power electronics.

3U CubeSat Frame
A custom-machined aluminum 3U CubeSat frame, designed to house satellite components within the standard 10 x 10 x 30 cm form factor.
| Mass | 0.350 kg |
| Dimensions | 10 × 10 × 10 cm |
Prosix Engineering
Spain · 2006 · 2 productsSpanish composites engineering company designing and manufacturing deployable carbon-fiber structures, antennas and instruments for space, aerospace, marine defense and marine racing applications.

Deployable Space Structures
Prosix offers a range of deployable space structures including masts, booms, and antenna reflectors, all utilizing advanced carbon fiber reinforced plastics for lightweight and hig
| Space deployable masts - length | 1 – 50 meters long |
| Space deployable masts - characteristics | Ultralight |
| Space deployable masts - characteristics (2) | Utracompact |
| Space deployable masts - characteristics (3) | High stiffness, accuracy and stability |
| Space deployable masts - characteristics (4) | Modular, Scalable |

Full Carbon Self-Deployable Booms
Ultralight, fully carbon-fiber articulated deployable boom from Prosix for reliably deploying instruments and tip-mass payloads such as reflectors or magnetometers.
| Deployed length | Up to 28 m |
| Material | 100% Carbon Fiber (Full CFRP) |
| Mechanism | Passive, damped self-deployment — no metallic mechanisms |
| Payload capability | Carries tip masses such as reflectors or magnetometers |
| Repeatability | Supports folding and unfolding multiple times at various velocities |
Pumpkin, Inc.
United States · 1995 · 20 productsSan Francisco-based manufacturer of flight-proven CubeSat kits, SUPERNOVA nanosatellite buses, and spacecraft power/electronics components, with over 150 kits delivered and dozens of successful space missions since 2003.

104-pin Bus Reversing Adapter
A development tool that allows a CubeSat Kit-compatible module to be installed upside-down on the 104-pin CubeSat bus, for testing modules lacking stackthrough connectors or for un
| Connector | 104-pin CubeSat bus, stackthrough on one side, standard header on reversed side |
| All pins passed through | 104 of 104 pins routed straight through |
| Included hardware | 3D-printed plastic support arms, miscellaneous M3 fasteners |

2nd Switch (L2) Spring Upgrade Kit
The 2nd Switch (L2) Spring Upgrade Kit provides hardware parts to enhance the spring strength of the second switch on Pumpkin base plate assemblies, compatible with Rev-E or later
| SKU | 711-01478 |
| Compatibility | Rev-E or later motherboard modules |
| Flight heritage | Flight Hardware | Flight Qualified | Space Proven |

ADACS Payload Walls / 1U Chassis MAI-100/MAI-200 Extension
CubeSat Kit structural walls that extend an MAI-100/200 ADCS unit into a 1U chassis section, enabling integration into larger multi-unit CubeSat structures.
| SKU | 703-00397 |
| Price | $1,610.00 per item |
| Status | Flight Hardware | Flight Qualified | Space Proven |
| Flight heritage | JPL/Stanford LMRST-Sat 3U mission |
| Operating temperature | -40 to +85 °C |

CubeSat Kit Quad-switch Cover Plate Assembly
A flight-qualified cover plate for CubeSat Kit structures permitting the use of up to four separation/inhibit switches, installable in any of four orientations at the top of the ch
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Mounting screws | Four M3 flathead stainless-steel screws |
| Number of switches | Four independent separation/inhibit switches (3 usable on standard CubeSat Kit chassis; 4 |
| Switch terminals | C, NC and NO solder terminals per switch |
| Style options | Solid-wall style, and style with 88 mm diameter central hole |

CubeSat Kit™ Base Plate Assembly
A precision aluminum end-plate assembly that forms the Motherboard Module (MBM)/C&DH end of a CubeSat Kit structure, available with single- or dual-independent separation switc
| Configuration option: type | Solid-Wall, Skeletonized |
| Configuration option: separation switch | Single (deprecated), Dual |
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Mounting fasteners | 6x M3 flathead stainless-steel screws |
| Separation switch terminals | C, NC, NO solder terminals per switch |

CubeSat Kit™ Base Plate Assembly for AntS Antenna
A base-plate assembly variant configured to mount a third-party AntS deployable antenna system, with dual independent separation switches, forming the Motherboard-Module end of a C
| Configuration option: separation switch | Dual |
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Mounting fasteners (to Chassis Walls) | 6x M3 flathead stainless-steel screws |
| Antenna compatibility | Third-party AntS deployable antenna system |
| Antenna mounting fasteners | 4x threaded fasteners |

CubeSat Kit™ Chassis Walls
Pumpkin's pioneering one-piece sheet-metal CubeSat structural element, available in 0.5U-3U sizes, that forms the primary chassis of a CubeSat Kit structure and defines its 97mm x
| Configuration option: size | 0.5U, 1U, 1.5U, 2U, 3U |
| Configuration option: type | Solid-Wall, Skeletonized |
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Internal cross-section | 97 mm x 97 mm |
| Construction | One-piece |

CubeSat Kit™ Cover Plate Assembly
A precision aluminum end-plate assembly that forms the payload end of a CubeSat Kit structure, secured to the Chassis Walls and fitted with four corner feet per the CubeSat Design
| Configuration option: type | Solid-Wall, Skeletonized |
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Mounting fasteners | 4x M3 flathead stainless-steel screws |
| Corner feet | 4 (included) |
| Options | Separation plungers in feet; additional separation switches in feet |

CubeSat Kit™ Cover Plate Assembly for AntS antenna
A cover-plate assembly variant configured to mount a third-party AntS deployable antenna system, with dual independent separation switches, forming one end of a CubeSat Kit structu
| Configuration option: separation switch | None, Dual |
| Antenna compatibility | Third-party AntS deployable antenna system |
| Antenna mounting fasteners | 4x threaded fasteners |
| Separation switch terminals | C, NC, NO solder terminals per switch |
| Price range (USD) | $955.00 - $1,085.00 |

CubeSat Kit™ Large Aperture Base Plate Assembly, Dual Switch
A precision-machined aluminum base plate assembly for the CubeSat Kit structure, designed for use with the Motherboard Module (MBM) C&DH subsystem and featuring dual switch fun
| SKU | 710-02203 |
| Price | $820.00 per item |
| Material | Al 5052-H32 |
| Plating | Per CubeSat Design Specification (CDS) |
| Attachment | Six M3 flathead stainless-steel screws to Chassis Walls |

CubeSat Kit™ Large Aperture Cover Plate Assembly
A CDS-compliant cover-plate assembly with an 88mm-diameter central cutout for payload-end apertures such as optics or antennas, with optional separation plungers and switches.
| Configuration option: separation switch | None, Dual |
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Mounting fasteners | 4x M3 flathead stainless-steel screws |
| Central cutout diameter | 88 mm |
| Corner feet | 4 (included) |

CubeSat Kit™ Payload Adapter Plate
A bulkhead plate used on the payload end of a CubeSat Kit structure to interface Pumpkin's sheet-metal Chassis Walls with a machined-aluminum external payload, enabling hybrid shee
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Mounting fasteners (to Chassis Walls) | 4x M3 flathead stainless-steel screws |
| Payload mounting | M3 bolt square pattern |
| Typical pairing | Payload Cover Plate Assembly (payload sandwiched between the two) |
| Price (USD) | $360.00 |

CubeSat Kit™ Payload Cover Plate Assembly
A CDS-compliant cover-plate assembly with four corner feet used on the payload end of a CubeSat Kit structure to interface a machined-aluminum external payload, typically paired wi
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Payload mounting | M3 bolt square pattern |
| Corner feet | 4 (included) |
| Typical pairing | Payload Adapter Plate (payload sandwiched between the two) |
| Price (USD) | $495.00 |

CubeSat Kit™ Pro Chassis Walls
The premium, higher-specification tier of Pumpkin's flight-proven one-piece sheet-metal CubeSat structural element, offered in 0.5U-3U sizes as Flight Hardware, Flight Qualified, S
| Configuration option: size | 0.5U, 1U, 1.5U, 2U, 3U |
| Product tier | Pro (premium variant of CubeSat Kit Chassis Walls) |
| Price range (USD) | $22,500.00 - $39,500.00 |

Mid-plane Standoff Kit
A hard-anodized aluminum standoff kit that couples the four threaded-rod columns of a CubeSat electronics module stack to the Chassis Walls, preventing lateral motion under vibrati
| Kit contents | 4 unique precision hard-anodized aluminum pieces + fastening hardware |
| Function | Couples threaded-rod columns of module stack to Chassis Walls; restrains X/Y motion under |
| Compatible chassis walls sizes | 1U, 1.5U, 2U, 3U (pre-drilled mounting holes); usable in 1U when space permits |
| Datasheet part number | 711-00331-B |
| Price (USD) | $200.00 |

Remove-Before-Flight (RBF) Bracket Kit
A precision aluminum bracket used in 1.5U/2U/3U CubeSat Kit structures to support and guide the Remove-Before-Flight pin, power connector and USB connector when the Motherboard Mod
| Material | Al 5052-H32, plated per CubeSat Design Specification (CDS) |
| Compatible chassis walls sizes | 1.5U, 2U, 3U |
| Mounting fasteners | 2x external M3 screws to Chassis Walls |
| Function | Guides RBF pin; supports external power and USB device connectors |
| Price (USD) | $165.00 |

Remove-Before-Flight (RBF) Pin and Lanyard
A Remove-Before-Flight (RBF) pin and lanyard used to engage the RBF pin/switch of a CubeSat Kit, keeping the satellite powered off during ground handling and integration.
| SKU | 710-00300 |
| Mass | 17 g |
| Price | $70.00 per item |
| Hardware classification | Development Hardware | Flight Hardware | Space Proven |
| DC current through Remove-Before-Flight or Separation Switch | 10 A |

Rod & Spacer Kit
A kit containing threaded rods and coaxial aluminum through-hole spacers designed to physically retain CubeSat Kit™ modules in a stack, adhering to the PC/104 specification.
| Mass | 4 g |
| Height | 5.0 mm |
| Mounting hole | M3 |
| Through hole | 3 mm |
| Material | Aluminum 7075-T6 |

Solar Panel Clips Set for AntS antenna
A set of clips designed to secure solar panels to the ISIS Antenna System (AntS) on CubeSats.
| Thickness | 0.031"/0.8 mm |
| Thickness (2) | 0.062"/1.6 mm |
| Maximum mass per panel (safety factor = 2) | 500 g |
| Mass | +9 g |
| Material thickness | 0.5 mm |

SUPERNOVA™ Structural Components
SUPERNOVA™ Structural Components are available from Pumpkin, Inc.
Roccor (Redwire)
United States · 1 productRedwire is an integrated aerospace and defense company that designs and manufactures advanced technologies for space and defense applications, including space infrastructure, autonomous systems, and m

Roccor Deployable Booms and Solar Array Structures
Roccor, part of Redwire Space, manufactures deployable composite booms, solar array support structures, and antenna deployment mechanisms for satellites ranging from CubeSats to la
| Products | Deployable booms, solar array structures, antenna mechanisms |
| Parent | Redwire Space |
Saransk Instrument-Making Plant
1 productSaransk Instrument-Making Plant (АО «Саранский приборостроительный завод») — Russian space industry enterprise, Saransk. Its products listed on NewSpace Market come from the Glavkosmos export catalogue.

SINGLE LAYER MEASURING BELLOWS
Single layer metal measuring bellows are flexible sensing elements designed for use in various measuring, monitoring, and control devices, particularly within automated control sys
| Purpose | Single layer metal measuring bellows are intended for operation as flexible sensing elemen |
| Year of release | 1959 |
| Design life | 6 years |
| Lead time | 2 months |
| Flight qualification of the product | No |
SENER Aeroespacial
Spain · 1956 · 2 productsSpanish engineering company supplying precision mechanisms, solar array drive assemblies, and structural components for ESA and commercial satellite missions.

ELT M5 Mirror Support Cell — Precision Space Mechanism by SENER
SENER Aeroespacial is a Spanish aerospace engineering company, part of the SENER Group, providing high-precision mechanisms, optical systems, and space structures for ESA, NASA, an
Space Mechanisms and Solar Array Systems
SENER Aeroespacial's precision space mechanisms — deployable solar array drives, antenna pointing mechanisms, hold-down and release systems for ESA and commercial satellites.
| Products | Solar array drives (SADM), antenna pointing mechanisms (APM), hold-down/release (HDRM) |
| Sadm feature | High-precision sun-tracking, 15+ year GEO lifetime |
| Actuation technology | Shape memory alloy (SMA), stepper motors, non-explosive releases |
| Mission heritage | Solar Orbiter, JUICE, Sentinel-1/2/3, Ariane 5/6 |
| HQ | Tres Cantos (Madrid), Spain / Bilbao, Spain |
Serenum Space
Czech Republic · 2020 · 1 productSERENUM Space is a CubeSat component and BUS manufacturer, integrator, and service provider based in Brno, Czech Republic, and a commercially oriented subsidiary of VZLU AEROSPACE.

Modular CubeSat Structures
Flight-heritage modular CubeSat structures (PC104-compatible, multi-size PCB support) in Aluminium/Titanium/Stainless Steel.
| Material options | Aluminium Alloy, Stainless Steel Alloy, Titanium Alloy |
| Compatibility | PC104 fully compatible, multiple PCB sizes supported |
| Thermal range | -40 to +60 °C |
| Safety feature | Dual kill-switch mechanism |
| Outside envelope (largest variant) | 226.3 x 100 x 340.5 mm |
Sheldahl (Multek Flexible Circuits)
United States · 1959 · 2 productsSheldahl (Multek Flexible Circuits) is a US manufacturer of flexible printed circuits, printed electronics, electronic materials, and aerospace thermal control materials, headquartered in Northfield, Minnesota.

Flexible Printed Circuits
Interconnect solutions that bend, fold, and conform to compact electronic and aerospace designs.
| Circuit types | Single-sided, double-sided, multi-layer |
| Fabrication process | Roll-to-roll automated processing |
| Via technology | Screen-thru-vias |
| Conductor options | Copper foil, printed silver flexible hybrid |
| Printed components | Printed resistors, printed piezo resistors |

Unidirectional Tapes
Sheldahl-branded unidirectional tapes and proprietary adhesive formulations for high-strength abrasive belts.
| Product forms | Unidirectional reinforcement tapes, coated tapes, adhesives/curatives |
| Core processes | Adhesive formulation, coating & laminating, perforating & embossing, slitting & sheeting |
| Primary application | Industrial abrasive belt reinforcement and bonding |
| Brand | Sheldahl-branded proprietary adhesive formulations |
Shenzhen MagicCubeSat Technology (MCS)
China · 2018 · 1 productShenzhen MagicCubeSat Technology (MCS) builds small satellites and their core onboard units, and operates remote sensing constellations. The company runs an automated production line for satellite core components in Chongqing with an annual

Solar Array Drive Assembly (SADA)
Solar array drive assembly for pointing deployable arrays at the Sun.
| Function | Solar array pointing drive |
| Application | Low-orbit small satellites |
Sidus Space, Inc.
United States · 2012 · 1 productUS space and defense technology company (NASDAQ: SIDU) building the LizzieSat multi-mission satellite platform, AI/ML edge-computing avionics, and precision satellite manufacturing services from its Florida Space Coast facilities.

Precision Manufacturing and Engineering Services
Sidus Space offers precision manufacturing, advanced avionics, and mission-critical hardware, alongside comprehensive design engineering services for space systems and subsystems.
| Flight heritage | Over 20 years |
| Certifications | ISO 9001:2015 / AS9100D |
Sierra Space
United States · 2021 · 6 productsUS commercial space company; Dream Chaser® cargo spaceplane, LIFE™ inflatable habitat modules, in-space manufacturing, and defense space systems spun off from Sierra Nevada Corporation.

C14 Bi-Axis Gimbal
The C14 Bi-Axis Gimbal from Sierra Space is a lightweight, bi-axial gimbal featuring the C14 incremental rotary actuator, developed specifically for critical spacecraft pointing ap
| Actuator | C14 Incremental Rotary Actuator |
| Applications | Antenna pointing, solar array drives, thruster/instrument pointing |
| Mass | 1.23 kg, excluding cables |
| Mass (2) | ~1.5 kg including 85 cm of cabling |
| Slew Rate | >9 degrees/s at no load |

EH25 Bi-Axis Gimbal, 3-Phase
The EH25 Bi-Axis Gimbal, 3-Phase from Sierra Space is an Enhanced Hybrid (EH25) gimbal with improved stiffness and torque capability closely modeled after the company’s stand
| Motor type | 3-Phase (Enhanced Hybrid) |
| Features | Single-step position telemetry, adjustable hard stops, internal heaters |

H25 Bi-Axis Gimbal, 4-Phase
The H25 Bi-Axis Gimbal, 4-Phase from Sierra Space features very fine pointing resolution, position telemetry precise to within a single step, adjustable hard stops, and extremely l
| Motor type | 4-Phase |
| Features | Single-step position telemetry, adjustable hard stops |

Hold Down Release Mechanism (HDRM)
Sierra Space’s Hold Down Release Mechanism (HDRM) is a fast-acting separation nut rated to accommodate several working preloads. The HDRM series uses a conventional segmented
| Trigger mechanism | Redundant shape memory alloy (SMA) |
| Reset time | <1 minute |
| Type | Non-pyrotechnic, field-resettable |

LDC20 Low-Disturbance Gimbal
Qualified bi-axis gimbal engineered for low-disturbance, open-loop operation in critical spaceflight pointing applications.
| Configuration | Bi-axis, open-loop |
| Status | Qualified for spaceflight |
| Mass | 8.2 kg |
| Resolution | 0.007 deg |
| Output Rotational Rate | 8 deg/s |

Lightweight 2-Axis Mini Gimbal
The Lightweight 2-Axis Mini Gimbal from Sierra Space is a simple X/Y gimbal designed for spacecraft requiring a small, fast-moving antenna or other payload. The interface brackets
| Configuration | X/Y 2-axis |
| Features | Removable interface brackets and cable wrap spools |
Skycorp Incorporated
United States · 1998 · 2 productsSkycorp designs the Orbital Logistics Vehicle, a reusable, on-orbit-assembled space platform with a standardized interface for hosting modular third-party payloads.

Intelligent Space Systems Interface (iSSI)
Standard, robotic on-orbit connector/bus interface providing power, data, bandwidth and physical rigidity for modular payload integration.

intelligent Space Systems Interface Flight Qualification Experiment (iSSI FQE)
On-orbit demonstrator of Skycorp's iSSI robotic connector, flown on ISS via NG-17 Cygnus, reached TRL-7.
| Launch vehicle/mission | NG-17 Cygnus (Northrop Grumman CRS-2) |
| Launch date | February 19, 2022 |
| Host platform | International Space Station (ISS) |
| On-orbit duration | Approximately 6 months |
| Technology readiness level achieved | TRL-7 |
Space Applications Services
Belgium · 1987 · 1 productBelgian engineering company delivering systems, products, and services for manned and unmanned spaceflight, robotics, mission control, and astronaut training.

HOTDOCK Mating/Demating Device
European standard mating/demating device for in-orbit servicing, assembly, and refuelling — recognised as a standard building block for OSAM missions.
| Type | Mechanical mating/demating device |
| Applications | In-orbit servicing (OSAM), assembly, refuelling, modular platforms |
| Configurations | Active and passive variants |
| Status | European standard building block (recognised by ESA) |
| Support | Full engineering, testing, and qualification services available |
Space Forge Limited
United Kingdom · 2018 · 1 productUK company (Cardiff, Wales) developing reusable in-space manufacturing platforms and a non-ablative reentry heat shield for producing semiconductor materials in microgravity.

Pridwen Heatshield
Pridwen is a novel heatshield designed for safe atmospheric re-entry and satellite recovery, utilizing a radiation-based thermal protection system and a shuttlecock-style design fo
| Design | Non-ablative, shuttlecock-style deployable heat shield |
| Function | Atmospheric reentry protection for in-space-manufactured payload recovery |
| Flight heritage | Parabolic flight deployment test (May 2025); operational on ForgeStar-1 (June 2025) |
Space Structures GmbH
Germany · 2011 · 3 productsGerman company (Berlin) providing structural engineering, analysis, and manufacturing of mechanical subsystems for spacecraft, including struts, sandwich panels, precision assemblies, and bolt/vibration analysis software.

Honeycomb Sandwich Panels
Custom honeycomb sandwich panels in aluminium, GFRP and CFRP face-skin/core combinations for satellite and launcher structures.
| Facesheet/core combinations | Aluminium/aluminium, GFRP/aluminium, CFRP/aluminium, CFRP/CFRP; NOMEX cores optional |
| Insert materials | Aluminium, titanium, INVAR, CFRP |
| Insert types | Floating, face-to-face, edge, block |
| Surface options | Anodising, surtec coating, black/white thermal paint, mirrors, surface-mounted or embedded |
| Applications | High-performance satellite and launcher structures, optical benches, sunshields |

Precision Assemblies
High-performance satellite and launcher structures, optical payload structures, and electronic equipment structures built to spec in-house.
| In-house processes | Bolting, riveting, bonding, alignment, measurement |
| Satellite/launcher structures | Primary/secondary structures, integrated radiator functionalities, launch vehicle adapters |
| Manned space applications | ISS, Orion, Lunar Gateway — fracture control and human-factors design |
| Optical payload structures | Telescope structures, optical benches, bipods/hexapods, straylight baffles |
| Electronic equipment structures | Power supply/control/distribution units, data handling/processing units |

SpaceStrut Struts and Booms
Family of lightweight, high-stiffness structural parts including struts, booms, rods, bars and beams with low thermal expansion.
| Hybrid strut construction | Composite tube (filament winding, thermoplastic, or prepreg) with metallic fittings (alumi |
| Full cfrp strut construction | Integral single CFRP piece with continuous fibres including fittings |
| Doublezero variant | Zero coefficient of thermal expansion and zero moisture expansion |
| Applications | Spacecraft primary structures, launcher structures, telescope structures, bipods/hexapods, |
SPUTNIX
Russia · 2011 · 1 productSPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.

Structure 1U CubeSat with Separation System
A 1U CubeSat structure designed for simple and fast assembly, providing a durable base for satellites with easy access to internal devices and supporting modular construction based
| Year of release | 2017 |
| Design life | 3 years |
| Lead time | 2 months |
| Flight qualification of the product | Yes |
| Brief history of flight qualification | In the composition of the satellites SiriusSat-1.2 (launched on 15.08.18.). |
Swiss Centre for Electronics and Microtechnology (CSEM)
Switzerland · 1984 · 1 productSwiss innovation and research center specializing in microelectronics, photonics, and digital technologies, with significant contributions to space and satellite instrumentation.

High-Precision Space Mechanisms
Flexure-based precision mechanisms for satellites, telescopes and planetary rovers — 30+ years heritage with ESA/NASA, flown on MTG, Metop, XMM and ExoMars.
| Precision | Micrometer-level, sub-micron resolution capable |
| Bearing type | Frictionless flexure structures |
| Operating environments | Cryogenic and vacuum |
| Fem analysis | COMSOL Multiphysics |
| Manufacturing | Conventional and additive (3D printed) with topological optimization |
TakeMe2Space
India · 2023 · 1 productIndia's first orbital compute company — building AI-first satellite infrastructure that captures, processes, and delivers Earth observation insights directly from LEO.

RadShield — Radiation Shielding Technology
Flight-validated tantalum-tape radiation shielding reducing TID up to 10x, enabling terrestrial-grade electronics for 5+ year LEO missions. Flown on PSLV C-58 (January 2024).
| Substrate material | 2 mm thick Aluminium AL 6061 |
| Coating material | Tantalum (Ta) tape |
| Coating thicknesses tested | 4, 50, and 100 microns |
| TID reduction | Up to 10x vs. unshielded components |
| Extended component life | 5+ years in LEO (vs. months uncoated) |
Tata Advanced Systems (Space)
India · 2006 · 3 productsTata Group aerospace and defense manufacturer providing satellite Assembly, Integration and Testing (AIT) services for ISRO and commercial operators

Composites
Tata Advanced Systems delivers composite components and assemblies for aerospace, aero-engines, space and defence applications, leveraging world-class manufacturing facilities and

Metallics
Tata Advanced Systems is a leading partner for machining and fabrication of complex aero-components, leveraging lean manufacturing and quality management systems.

Satellite Structure Assembly and Integration
Advanced composite and metallic satellite structures and spacecraft assembly services from Tata Advanced Systems, supporting Indian and global satellite programs.
| Products | Composite structures, metallic components, spacecraft assembly |
| Customers | ISRO, commercial satellite manufacturers |
| Country | India |
TechTheMoon
France · 2021 · 1 productThe world's first incubator dedicated exclusively to the Moon, backed by CNES, supporting entrepreneurs developing solutions for sustainable human presence on the lunar surface.
Spartan Space EuroHab/ILOT — Inflatable Lunar Habitat
Spartan Space, incubated by TechTheMoon, is developing inflatable space habitats for lunar exploration and underwater environments. The EuroHab/ILOT concept is designed as a lunar
| Type | Inflatable lunar habitat |
| Deployment | Lunar lander payload |
| Key advantage | Higher habitable volume-to-mass ratio vs. rigid structures |
| Mobility | Surface mobility capability included |
| Analog | Underwater variant for space analog missions |
Tethers Unlimited, Inc. (AMERGINT)
United States · 1994 · 3 productsUS developer of deployable space structures, the SWIFT software-defined radio, HYDROS water-electrolysis thrusters and in-space manufacturing tech; now part of ARKA Group (formerly AMERGINT).

COBRA-HPX Gimbal
Space-qualified 3-DOF (az/el/thrust) pointing gimbal using the Canfield-Joint carpal-wrist design for full-hemisphere, singularity-free antenna pointing.
| Mass | 276 g |
| Pointing resolution | ≥ 276 arc-sec |
| Repeatability | ≤ ± 276 arc-sec |
| Stowed footprint | 113 mm ⌀ |
| Stowed height | 29 mm |

COBRA™ Gimbal
The COBRA Gimbal is a 3DOF (azimuth, elevation, thrust) pointing mechanism that uses a Canfield Joint carpal-wrist design for precise, full-hemisphere pointing capability.
| Flight heritage | ! |
| Cobra-hpx™ mass | 276 g |
| Cobra-hpx™ pointing resolution | ≥ 276 arc-sec |
| Cobra-hpx™ repeatability | ≤ ± 276 arc-sec |
| Cobra-hpx™ stowed footprint | 113 mm ø |

KRAKEN Robotic Arm
Compact 7-DOF, 1-meter robotic manipulator with a hot-swappable end-effector interface and per-joint force sensing, for in-space assembly, manufacturing and servicing.
| Degrees of freedom | 7 DOF |
| Arm length | 1 m (standard configuration) |
| Stowed volume | 19 cm x 27 cm x 36 cm |
| End effector | Hot-swappable end-effector interface |
| Joint sensing | High-speed force sensing in each joint; embedded controller with force-control capability |
Tetonsys
United States · 2013 · 1 productUS CubeSat and PocketQube deployer maker at NASA Research Park, Moffett Field CA, founded 2013; composite structures, in-space 3D printing research; Gauss Team launch partner.

PocketQube Satellite Structure
Standard PocketQube satellite structures in 1P, 2P, and 3P sizes for launch via the MR-FOD deployer.
| Form factors | 1P, 2P, 3P PocketQube |
| Compatible deployer | MR-FOD |
| Launch platform | Italian UniSat micro-satellite |
Thermavant
United States · 2007 · 3 productsUS oscillating heat pipe (OHP) thermal management company; heat frames, chassis, radiators, and cold plates for space, airborne, and high-temperature electronics applications.

Cold Plates
Single- and two-phase pumped fluid cold plates for high-power electronics, from simple welded and inlaid-tube designs to complex brazed microchannel plates, optionally combined wit
| Materials | Al and Al composites (0 to T6 temper, most common); Cu and Cu composites incl. Copper-Moly |
| Working fluids | Deionized water (with corrosion inhibitors and internal channel chem film); EGW; PGW; PAO |
| Heat flux capability | Up to 50 W/cm² (higher when integrated with an oscillating heat pipe) |
| Operating temperature range | Fluid-dependent, from cryogenic to traditional electronics-cooling temperatures to interme |
| Shapes and sizes | From less than 1 mm thickness up to 2 m length; customizable widths from < 2 cm to > 1 m; |

OHP Chassis
Oscillating heat pipe (OHP) embedded electronics chassis and enclosures that structurally house circuit cards, RF modules, and Li-ion cells while conducting heat directly to spacec
| Simple chassis example thermal performance (OHP) | 11 °C rise per 120 W |
| Simple chassis example thermal performance (solid Al) | 35 °C rise per 120 W (3.2x worse than OHP) |
| Simple chassis example mass (OHP) | 995 g |
| Simple chassis example mass (solid Al) | 1,049 g (1.1x worse than OHP) |
| Simple chassis shape & structure | Al 6061 T4/T6, approx. 12" x 8" x 1.0" thick, min. 0.1" thickness at center |

OHP Heat Frames
Oscillating heat pipe (OHP) embedded structural heat frames for VPX/VITA circuit cards and RF/power electronics, offering up to 3x-5x the thermal conductance of solid aluminum with
| 3u example thermal performance (OHP) | 10 °C rise per 130 W |
| 3u example thermal performance (solid Al) | 30 °C rise per 130 W (3x worse than OHP) |
| 3u example thermal performance (solid Cu) | 14 °C rise per 130 W (1.4x worse than OHP) |
| 3u example mass | 135 g (Al 6061 T4 w/ ChemFilm) |
| 3u shape & structure | Standard VITA 3U (~3.9" x 5.9"), min. thickness 0.06", equipped with COTS wedgelocks |
ThinkOrbital, Inc.
United States · 2021 · 1 productUS space infrastructure company developing large, single-launch, autonomously-assembled spherical orbital modules (ThinkPlatform) and an in-space construction/welding and X-ray inspection toolkit (ThinkToolkit).

ThinkToolkit
Robotic arm and arm-agnostic end-effector suite for in-space servicing, construction, and inspection, including flight-proven electron-beam welding.
| Welding method | Electron beam welding |
| Weld capacity | 30 cm of steel in a single pass |
| Energy efficiency | > 90% |
| Environment requirement | High vacuum |
| Components | Robotic arm plus arm-agnostic end effector |
Toray Industries Space
Japan · 1926 · 2 productsJapanese advanced materials manufacturer supplying carbon fiber composites for launch vehicles and spacecraft.
Carbon Fiber Composites for Space Structures
Toray Industries' high-modulus carbon fiber and CFRP composite materials used in satellite primary structures, rocket motor cases, fairing panels, and solar array substrates.
| Key products | T700SC/T800 carbon fibers, M-grade high-modulus fibers (M46J, M55J, M60J), CFRP prepregs |
| M-grade stiffness | 450–600 GPa (vs. 210 GPa for steel) |
| Applications | Satellite primary structures, fairings, motor cases, solar array substrates |
| Launch vehicle programs | Ariane 6 fairings, solid motor cases, interstages |
| Space-specific advantage | Dimensional stability — no thermal expansion distortion of optical/antenna structures |

Toray TC380 Epoxy Prepreg
High-modulus aerospace-grade epoxy prepreg for primary spacecraft structures — intermediate cure at 121°C, exceptional hot/wet mechanical properties, widely used in satellite panel
| Resin system | Epoxy (TC380) |
| Cure temperature | 121°C (250°F) |
| Tg (dry) | ~170°C |
| Tg (wet) | ~135°C |
| Out-life at 21°c | >21 days |
TransAstra
United States · 2017 · 1 productTrans Astronautica Corporation (TransAstra) is a deep space technology company pioneering in-space logistics and asteroid mining. Founded in 2017 and backed by NASA, DARPA, AFRL, Space Force, and Y Combinator, TransAstra develops capabiliti

Mantis Capture Bag™
The Mantis Capture Bag™ is a lightweight, durable, and inflatable structure for orbital debris cleanup and the capture of uncooperative space objects. Successfully demonstrated on
TRL Space
Czech Republic · 2014 · 1 productCzech mission integrator and space hardware builder behind the CAVE CubeSat deployer, TRONE/CRUSOE EGSE, and the TRACE/TROLL NG/TRULY satellite missions.

Prusament PC Space Grade Black
Prusament PC Space Grade Black is an ESD-safe, low-outgassing polycarbonate filament engineered for functional parts and ground support components in space and vacuum environments.
| Tensile strength | 75 MPa |
| Tensile modulus | 3.7 GPa |
| Outgassing (ESA) tml | 0.25 % |
| Outgassing (ESA) rml | 0.12 % |
| Outgassing (ESA) cvcm | 0.00 % |
VACCO Industries
United States · 1954 · 8 productsUS manufacturer of precision fluid control components and integrated propulsion systems for spacecraft, with 70+ years of heritage. Products include micro propulsion systems, valves, pressure regulators, and CubeSat propulsion modules.

4500 Series Tee Type Filter Single Stage 3000 psi
A series of single-stage tee type filters designed for 3000 psi operating pressure, with various connection types and sizes.
| Operating pressure | 3000 PSIG |
| Max element pressure drop | 10 psi |
| Operating temperature (Buna-N) | -65 °F to 225 °F |
| Operating temperature (Propylene) | -65 °F to 300 °F |
| Operating temperature (Viton) | -20 °F to 350 °F |
VACCO F1D10286-02 etched disc filter
A 2 micron absolute etched disc filter made from Titanium alloy.
| Materials of construction | Titanium alloy |
| Filtration | 2 micron absolute |
| Type of media | Etched Discs |
| Meop / proof pressure / burst pressure | 4200 / 6300 / 16800 psi |
| Delta p and flow | 0.30 psid @ 0.0113 scfm of GN2 @ 295 psig & 70 °F (actual test result); 6.5 psid (cal) @ 0 |
VACCO F1D10588-01 Etched Disc Filter
A high pressure, low gas flow miniature etched disc filter made from titanium alloy, providing 40 micron absolute filtration.
| Materials of construction | Titanium alloy |
| Filtration | 40 micron absolute |
| Type of media | Etched Discs |
| Meop / proof pressure / burst pressure | 4350 / 8700 / 17400 psi |
| Leakage | < 1.0 x 10-6 sccs GHe at MEOP external |
VACCO F1D10636-01 Etched Disc Filter
A high pressure, low gas flow etched disc filter made from CRES 304L, providing 10 micron absolute filtration.
| Materials of construction | CRES 304L |
| Filtration | 10 micron absolute |
| Type of media | Etched Discs |
| Meop / proof pressure / burst pressure | 4800 / 7200 / 12000 psi |
| Leakage | < 1.0 x 10-6 sccs GHe at MEOP external |
VACCO F1D10638-01 Etched Disc Filter
A low liquid flow etched disc filter made from titanium alloy, providing 15 micron absolute filtration.
| Materials of construction | Titanium alloy |
| Filtration | 15 micron absolute |
| Type of media | Etched Discs |
| Meop / proof pressure / burst pressure | 600 / 900 / 1500 psi |
| Leakage | < 1.0 x 10-6 sccs GHe at MEOP external |

VACCO F1D10639-01 Etched Disc filter
A medium liquid flow Etched Disc filter made from CRES 304L, providing 15 micron absolute filtration.
| Materials of construction | CRES 304L |
| Filtration | 15 micron absolute |
| Type of media | Etched Discs |
| Meop / proof pressure / burst pressure | 500 / 750 / 1250 psi |
| Leakage | < 1.0 x 10-6 sccs GHe at MEOP external |
VACCO F1D10784-01 etched disc filter for Xenon application
A 5 micron absolute etched disc filter made from Titanium alloy, specifically for Xenon applications.
| Materials of construction | Titanium alloy |
| Filtration | 5 micron absolute |
| Type of media | Etched Discs |
| Meop / proof pressure / burst pressure | 2610 / 5220 / 10440 psi |
| Delta p and flow | 1.45 psid max. @ 0.20 mg/s of xenon @ MEOP |
VACCO F1D10807-02 Etched Disc Filter
A low liquid flow miniature etched disc filter made from titanium alloy, providing 15 micron absolute filtration.
| Materials of construction | Titanium alloy |
| Filtration | 15 micron absolute |
| Type of media | Etched Discs |
| Meop / proof pressure / burst pressure | 300 /1000 / 12500 psi |
| Leakage | < 1.0 x 10-6 sccs GHe at MEOP external |
VENG S.A.
Argentina · 2007 · 1 productArgentine space engineering company (Buenos Aires, founded 2007) and prime contractor to CONAE for the Tronador II launch vehicle programme, satellite avionics, propulsion, and ground-segment systems.

Tanques soldados por Friction Stir Welding (FSW)
Friction Stir Welded (FSW) pressurized aluminum 2219 propellant tank structures developed by VENG for the first stage of the Tronador II-250 space launch vehicle.
| Prototype tank length | 3.5 m |
| Prototype tank diameter | 2.5 m |
| Prototype tank wall thickness | 3.2 mm |
| Tank material | Aluminum 2219 (space grade) |
| Welding standard | American Welding Society (AWS) international standards |
Directory
Manufacturers in this sector
2NDSpace Srl
New Space company designing modular nanosatellite/CubeSat hardware: structures, solar panels, EPS, antennas, OBCs, and deployers/separation systems.
AAC Clyde Space
AAC Clyde Space provides small satellite technologies and space-based data services, offering end-to-end solutions from satellite components to data analytics for various applications.
AADYAH Aerospace
Aerospace company supporting space exploration missions; partners with ISRO, Skyroot, Orbex, Bellatrix, and Latitude on lunar and Mars programmes.
ACT (Advanced Cooling Technologies)
Premier thermal management solutions company specializing in custom two-phase heat transfer technology for aerospace, defense, and industrial applications.
Adaptive Launch Solutions
Adaptive Launch Solutions (ALS) provides launch integration services and designs adaptive structures and avionics for multi-manifesting pico to small satellites on various launch vehicles.
Alba Orbital
Alba Orbital manufactures PocketQube satellites, provides launch and ground station services, and operates a fleet of nighttime imaging satellites for government and commercial clients.
Aphelion Orbitals
Aphelion Orbitals is a New Jersey-based launch vehicle company developing the Helios nanosatellite launch system for regular, scheduled orbital access at low cost.
Arquimea
Spanish space technology company founded 2007 in Leganes, developing MEMS relay switches, SiC power devices, and miniaturized power conditioning units for satellite applications.
Astrix Astronautics
Astrix Astronautics provides inflatable space deployment systems for solar arrays, radiators, antennas, drag sails, and heat shields, offering high surface area and mass efficiency.
AstroForge
AstroForge is a deep-space mining company that builds spacecraft to track and extract valuable metals from asteroids, aiming to integrate space resources into Earth's supply chain.
Astronika
Astronika is a Polish space mechanisms company and ESA/NASA mission supplier, developing deployable booms, hold-down mechanisms, penetrating devices, and precision actuators for science and
Astroscale US
Pioneer in space debris removal and satellite life extension services, developing rendezvous, proximity operations, and capture technologies to ensure sustainable orbital environments.
Azimut Space
Azimut Space GmbH is a Berlin-based space engineering SME with 15+ years of experience in thermo-mechanical engineering, developing thermal control systems, payloads, scientific instruments,
Beyond Gravity (ex-RUAG Space)
Swiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.
Boltless CubeSat Structures (Kikuchiseiki, KIKUCHI SEIKI)
Kikuchi Seiki provides high-precision metalworking services, including machining, fabrication, and assembly, specializing in components for various industries, including aircraft engines.
Comat
Comat is a French aerospace equipment manufacturer, part of the Hemeria group, designing flight hardware and mechanisms for small satellites, telecommunications/observation payloads, and spa
Compoxi
Compoxi is a Spanish composite design and manufacturing company delivering turnkey carbon-fiber and glass-fiber structures for space, aeronautics, and industrial applications, including sate
CTD (Composite Technology Development)
CTD develops state-of-the-art composites for extreme conditions and demanding applications in aerospace, high performance magnets, cryogenic systems, marine, automotive, and industrial secto
CubeSat Aerospace
Indian CubeSat developer offering flight-ready 1U–6U satellite structures, subsystem components, environmental testing services, launch integration, and STEM education programs from Ahmedaba
Data Patterns (India) Ltd.
Vertically integrated Indian defence and aerospace electronics company designing and manufacturing avionics, microelectronics, RF/microwave, radar, test equipment and space systems.
Dcubed
German manufacturer of space deployables using patented Shape Memory and Origami technologies — release actuators, solar arrays, and antenna deployables for CubeSats and microsatellites.
DeltaV Robotics
DeltaV Robotics was founded by Niha Agarwalla and Naushad Rahman, who have experience in commercial and defense space, including flight-proven spacecraft engineering.
DELTAV Space Technologies
Turkish aerospace company developing hybrid rocket propulsion, cryogenic systems, composite structures, and in-space propulsion — with a sounding rocket exceeding 200 km altitude and a hybri
Deployable Space Systems (DSS) — now Redwire
Deployable Space Systems (DSS), now part of Redwire, develops and produces the ROSA (Roll-Out Solar Array) — the deployable solar wing powering ISS upgrades, DART, and the Gateway PPE.
EIE Space Technologies Srl
EIE Space Technologies Srl operates in the Space sector. The company designs and manufactures support equipment for model testing.
ElmSpace
Developer of fluid-dynamic attitude control systems, gyroscopes, and air bearings for the space industry.
Enduralock
Enduralock creates a full-scale solution for satellite providers to refuel, upgrade, repair, and assemble assets directly in orbit. They engineer servicing and assembly components for satell
EnduroSat
Software-flexible CubeSat platforms (1U–16U+), shared-satellite hosted-payload service.
Ensign-Bickford Aerospace & Defense (EBAD)
US manufacturer of non-explosive actuators (TiNi FrangiBolt, pin pullers, ejectors) and energetic hold-down and release systems.
Exolaunch
Berlin-based launch and deployment services company providing end-to-end rideshare missions, satellite integration, and proprietary separation hardware for small satellites.
FAULHABER Drive Systems
FAULHABER Drive Systems manufactures DC-Motors, Brushless DC-Motors, Motors with integrated Electronics, Stepper Motors, Linear Motors, Precision Gearheads, Linear Actuators, Encoders, and D
Froberg Aerospace
Developer of multimode chemical-electric propulsion systems for small satellites.
Frond Space Systems
Frond Space Systems is a New Zealand space technology company specialising in satellite deorbiting solutions, bus platforms, and subsystem components for the CubeSat and small satellite mark
Gama Space
Gama Space develops solar sail propulsion for low-cost deep space missions and Astrobrake, an autonomous drag sail for satellite deorbiting compliance.
GITAI
GITAI develops robotic technologies for space exploration, including solutions for satellite construction, lunar settlements, and Martian cities, with a robot currently on the ISS.
GomSpace
GomSpace is a Danish CubeSat manufacturer producing satellite platforms, subsystems, and end-to-end mission solutions. Products include the NanoCom radio modules, NanoPower EPS, and complete
Gran Systems
System integrator and manufacturer of CubeSat structures, buses, and MyPOD test/transport pods, with space environment test equipment services.
Harmonic Drive
Harmonic Drive produces high precision gears, actuators, and servo drives. They offer rotary actuators, linear actuators, integrated actuators, gear units, and component sets.
Hemeria
HEMERIA designs, produces, and supplies space systems, vehicles, and defense equipment for commercial, institutional, and scientific customers.
HPS High Performance Space Structure Systems
HPS designs, manufactures, and integrates mechanical/thermal space subsystems, including antennas, deployable structures, thermal insulation, and equipment for nanosatellites.
ISISPACE Group
CubeSat deployers, antennas, EPS and small-satellite systems.
Kairo Space
South Korean nanosatellite manufacturer offering CubeSat platforms, optical imagers, star trackers, solar panels, EPS, structures, and deployers for the commercial small satellite market.
Kall Morris Inc
Kall Morris Inc provides in-space logistics, scavenging, and long-haul transport solutions, developing spacecraft and systems for satellite mobility and orbital debris management.
Kayser Space
Kayser Space designs, manufactures, integrates, and tests hardware and platforms for space programs, supporting over 100 missions and microgravity research.
KOSMOLAB Launch Services
CubeSat & small-satellite rideshare brokerage — integration, paperwork, launch insurance on PSLV, Falcon 9 Transporter, Ariane 6 and Soyuz.
KSF Space Foundation
USA non-profit democratizing access to space technology by offering affordable CubeSat and nanosatellite hardware, suborbital launch services, near-space missions, and professional space eng
L.Garde Inc
L.Garde designs, develops, and manufactures inflatable and deployable structures for space and terrestrial applications, including solar sails and advanced observation structures.
Lamb Space Tec
Polish manufacturer of small satellites, CubeSat components, and subsystems for Earth observation and communications missions.
Large Space Structures GmbH
Large Space Structures GmbH designs and manufactures large deployable reflector technologies for space applications, including LDRs and deployable antennas.
materion
Materion designs and manufactures advanced materials, including specialty alloys, chemicals, metals, beryllium composites, and optical coatings, for various industries including aerospace an
MDA Space
MDA Space designs and manufactures robotics, satellite systems, and provides geointelligence services for the global defense and space industry.
Media Lario
Media Lario produces optical components and systems for space telescopes, satellite earth observation systems, and laser optical communications systems. Their products include optical system
Memetis
Memetis GmbH designs and manufactures ultracompact microvalves and highly integrated microfluidic systems for space, life science, and medical technology applications.
Micromotion GmbH
Micromotion GmbH designs and manufactures high-precision micro drive technology, including micro drives and micro gearboxes, for various applications including space technology.
MinoSpace
Chinese commercial satellite manufacturer building Earth observation, communications, and remote sensing satellites, plus payloads, components, and ground terminal systems.
MMA Design
MMA Design manufactures deployable solutions for space and terrestrial missions, including de-orbit systems and solar arrays, and is headquartered in Broomfield, Colorado.
Moog Space Defense Group
Precision motion control and propulsion systems provider for space and defense applications.
Motiv Space Systems
Motiv Space Systems designs and builds space robotics, motor controllers, and mechanisms, including the robotic arm on NASA's Mars 2020 Perseverance rover.
MT Aerospace
German aerospace components manufacturer producing satellite tanks, CFRP structures, and antenna dishes for European satellite programs.
NanoAvionics
Pre-integrated nanosatellite buses (3U–16U+ MP42), green chemical propulsion, mission integration.
NazarX
Uzbekistan's first private aerospace engineering research and development center, building rocket prototypes, modular satellite platforms, and running national space-education programs.
Nimesis Technology
Nimesis Technology designs and manufactures space actuators and mechanisms using shape memory alloys for satellites, launchers, and other space applications.
Northrop Grumman Space Systems
Minotaur family, Pegasus XL, Antares (legacy); MLV co-development with Firefly.
NPC Spacemind
NPC Spacemind designs and manufactures CubeSat separation systems, deployers, and subsystems, including deorbiting systems, for nanosatellites and CubeSats.
Opterus Research and Development
U.S. manufacturer of deployable spacecraft structures and subsystems - booms, solar arrays and RF antennas - built on proprietary high-strain composite and origami-inspired technology.
Orbital Composites
Robotic additive manufacturing company producing high-performance composite parts for aerospace, defense and space applications at scale.
Orbital Matter
In-space manufacturing company building 3D-printing hardware that constructs large structural booms and infrastructure directly in orbit.
Orbotic Systems
Orbotic Systems designs spacecraft protection, control, and orbital lifecycle management technologies, including drag-based deorbit devices, onboard threat-detection systems, and non-coopera
PacSci EMC
PacSci EMC designs and manufactures mission-critical pyrotechnic and energetic material devices and integrated systems for aerospace, defense, energy and space applications.
Perigee Aerospace
South Korean small launch vehicle company developing the liquid-methane Blue Whale rocket family and in-house propulsion systems.
Phytron GmbH
Phytron GmbH manufactures stepper motors, end stages, controllers, mechanics, and equipment. They develop drive solutions for various applications, including those requiring high precision a
PIAP Space
Polish robotics and space technology company developing robotic systems, space mechanisms, and rover technologies for planetary exploration and satellite servicing missions.
Plan-S (Connecta)
Plan-S designs, manufactures, launches, and operates satellite systems for IoT connectivity (Connecta) and Earth observation data analytics (Observa), with 21 satellites launched.
Princeton Satellite Systems
Advanced aerospace and energy technology company specializing in spacecraft GN&C software toolboxes, satellite design tools, fusion propulsion research (Starfire/DFD), CubeSat hardware, and
Prosix Engineering
Spanish composites engineering company designing and manufacturing deployable carbon-fiber structures, antennas and instruments for space, aerospace, marine defense and marine racing applica
Pumpkin, Inc.
San Francisco-based manufacturer of flight-proven CubeSat kits, SUPERNOVA nanosatellite buses, and spacecraft power/electronics components, with over 150 kits delivered and dozens of success
Roccor (Redwire)
Redwire is an integrated aerospace and defense company that designs and manufactures advanced technologies for space and defense applications, including space infrastructure, autonomous syst
Saransk Instrument-Making Plant
Saransk Instrument-Making Plant (АО «Саранский приборостроительный завод») — Russian space industry enterprise, Saransk. Its products listed on NewSpace Market come from the Glavkosmos expor
SENER Aeroespacial
Spanish engineering company supplying precision mechanisms, solar array drive assemblies, and structural components for ESA and commercial satellite missions.
Serenum Space
SERENUM Space is a CubeSat component and BUS manufacturer, integrator, and service provider based in Brno, Czech Republic, and a commercially oriented subsidiary of VZLU AEROSPACE.
Sheldahl (Multek Flexible Circuits)
Sheldahl (Multek Flexible Circuits) is a US manufacturer of flexible printed circuits, printed electronics, electronic materials, and aerospace thermal control materials, headquartered in No
Shenzhen MagicCubeSat Technology (MCS)
Shenzhen MagicCubeSat Technology (MCS) builds small satellites and their core onboard units, and operates remote sensing constellations. The company runs an automated production line for sat
Sidus Space, Inc.
US space and defense technology company (NASDAQ: SIDU) building the LizzieSat multi-mission satellite platform, AI/ML edge-computing avionics, and precision satellite manufacturing services
Sierra Space
US commercial space company; Dream Chaser® cargo spaceplane, LIFE™ inflatable habitat modules, in-space manufacturing, and defense space systems spun off from Sierra Nevada Corporation.
Skycorp Incorporated
Skycorp designs the Orbital Logistics Vehicle, a reusable, on-orbit-assembled space platform with a standardized interface for hosting modular third-party payloads.
Space Applications Services
Belgian engineering company delivering systems, products, and services for manned and unmanned spaceflight, robotics, mission control, and astronaut training.
Space Forge Limited
UK company (Cardiff, Wales) developing reusable in-space manufacturing platforms and a non-ablative reentry heat shield for producing semiconductor materials in microgravity.
Space Structures GmbH
German company (Berlin) providing structural engineering, analysis, and manufacturing of mechanical subsystems for spacecraft, including struts, sandwich panels, precision assemblies, and bo
SPUTNIX
SPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.
Swiss Centre for Electronics and Microtechnology (CSEM)
Swiss innovation and research center specializing in microelectronics, photonics, and digital technologies, with significant contributions to space and satellite instrumentation.
TakeMe2Space
India's first orbital compute company — building AI-first satellite infrastructure that captures, processes, and delivers Earth observation insights directly from LEO.
Tata Advanced Systems (Space)
Tata Group aerospace and defense manufacturer providing satellite Assembly, Integration and Testing (AIT) services for ISRO and commercial operators
TechTheMoon
The world's first incubator dedicated exclusively to the Moon, backed by CNES, supporting entrepreneurs developing solutions for sustainable human presence on the lunar surface.
Tethers Unlimited, Inc. (AMERGINT)
US developer of deployable space structures, the SWIFT software-defined radio, HYDROS water-electrolysis thrusters and in-space manufacturing tech; now part of ARKA Group (formerly AMERGINT)
Tetonsys
US CubeSat and PocketQube deployer maker at NASA Research Park, Moffett Field CA, founded 2013; composite structures, in-space 3D printing research; Gauss Team launch partner.
Thermavant
US oscillating heat pipe (OHP) thermal management company; heat frames, chassis, radiators, and cold plates for space, airborne, and high-temperature electronics applications.
ThinkOrbital, Inc.
US space infrastructure company developing large, single-launch, autonomously-assembled spherical orbital modules (ThinkPlatform) and an in-space construction/welding and X-ray inspection to
Toray Industries Space
Japanese advanced materials manufacturer supplying carbon fiber composites for launch vehicles and spacecraft.
TransAstra
Trans Astronautica Corporation (TransAstra) is a deep space technology company pioneering in-space logistics and asteroid mining. Founded in 2017 and backed by NASA, DARPA, AFRL, Space Force
TRL Space
Czech mission integrator and space hardware builder behind the CAVE CubeSat deployer, TRONE/CRUSOE EGSE, and the TRACE/TROLL NG/TRULY satellite missions.
VACCO Industries
US manufacturer of precision fluid control components and integrated propulsion systems for spacecraft, with 70+ years of heritage. Products include micro propulsion systems, valves, pressur
VENG S.A.
Argentine space engineering company (Buenos Aires, founded 2007) and prime contractor to CONAE for the Tronador II launch vehicle programme, satellite avionics, propulsion, and ground-segmen
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