Structures & Mechanisms

New Space company designing modular nanosatellite/CubeSat hardware: structures, solar panels, EPS, antennas, OBCs, and deployers/separation systems.

2NDSpace Srl

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

price on requestdatasheet

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.

AAC Clyde Space

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

price on requestdatasheet

Aerospace company supporting space exploration missions; partners with ISRO, Skyroot, Orbex, Bellatrix, and Latitude on lunar and Mars programmes.

AADYAH Aerospace

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

price on request

Premier thermal management solutions company specializing in custom two-phase heat transfer technology for aerospace, defense, and industrial applications.

ACT (Advanced Cooling Technologies)

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

price on request

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.

Adaptive Launch Solutions

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

price on request

Alba Orbital manufactures PocketQube satellites, provides launch and ground station services, and operates a fleet of nighttime imaging satellites for government and commercial clients.

Alba Orbital

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.

Size	1P (Unit) - 50mm x 50mm external dimensions. 47mm x 47mm internal dimensions (widest point
Flight Heritage	Earlier version has Flight Heritage

price on requestdatasheet

Alba Orbital

2P Skeleton Wall PocketQube Structure

A skeletonized wall structure designed for the PocketQube Standard (Pico-satellite class), made from aerospace-grade aluminum.

Size	2P (Unit)
External dimensions	114mm x 50mm x 50mm
Internal dimensions (widest point)	114mm x 47mm x 47mm
Manufacturer	Alba Orbital
Flight Heritage	Earlier version has Flight Heritage

price on requestdatasheet

Alba Orbital

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

Size	3P (Unit)
External dimensions	178mm x 50mm x 50mm
Internal dimensions (widest point)	178mm x 47mm x 47mm
Manufacturer	Alba Orbital
Delivery time	8 weeks depending on available stock levels (much sooner if in stock)

price on requestdatasheet

Alba Orbital

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.

Size	1p,1.5p,2p,2.5p (Unit)
Price	£9,999.00
Delivery time	4 weeks depending on available stock levels (much sooner if in stock)
Datasheet/Brochure	Coming Soon

£9 999

Alba Orbital

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.

price on request

Aphelion Orbitals is a New Jersey-based launch vehicle company developing the Helios nanosatellite launch system for regular, scheduled orbital access at low cost.

Aphelion Orbitals

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	113.5mm
Width	100mm
Depth	100mm
Material	7075-T651
Mass	92g

price on request

Spanish space technology company founded 2007 in Leganes, developing MEMS relay switches, SiC power devices, and miniaturized power conditioning units for satellite applications.

Arquimea

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)
Temperature range	-40°C to +100°C
Solar panel stowed separation	20 mm from spacecraft to panel
Deployment detection	Sensor detects start and end of deployment

price on request

Arquimea

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

price on request

Former Spanish space engineering company; merged into ARQUIMEA Group. IberEspacio.es now redirects to arquimea.com.

Astrix Astronautics provides inflatable space deployment systems for solar arrays, radiators, antennas, drag sails, and heat shields, offering high surface area and mass efficiency.

Astrix Astronautics

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

price on request

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.

AstroForge

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)

price on request

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 commercial satellite missions.

Astronika

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

price on request

Pioneer in space debris removal and satellite life extension services, developing rendezvous, proximity operations, and capture technologies to ensure sustainable orbital environments.

Astroscale US

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

price on request

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, and ground support equipment for satellite, instr

Azimut Space

Thermal Strap / Thermal Link

Custom flexible thermally conductive links made of copper, aluminium, or Pyrolytic Graphite Sheets for precise heat management in space applications.

price on request

Kikuchi Seiki provides high-precision metalworking services, including machining, fabrication, and assembly, specializing in components for various industries, including aircraft engines.

Boltless CubeSat Structures (Kikuchiseiki, KIKUCHI SEIKI)

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)

price on request

Comat 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.

Comat

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

price on request

Compoxi 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

Compoxi

Composite Radomes for Launchers and Satellites

Glass-fiber reinforced polymer (GFRP) radomes manufactured for European launch vehicles and for LEO/GEO orbit satellites.

price on request

Compoxi

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

price on request

Compoxi

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.

price on request

Compoxi

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

price on request

CTD develops state-of-the-art composites for extreme conditions and demanding applications in aerospace, high performance magnets, cryogenic systems, marine, automotive, and industrial sectors.

CTD (Composite Technology Development)

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

price on requestdatasheet

CTD (Composite Technology Development)

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

price on request

CTD (Composite Technology Development)

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

price on request

CTD (Composite Technology Development)

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

price on requestdatasheet

Indian CubeSat developer offering flight-ready 1U–6U satellite structures, subsystem components, environmental testing services, launch integration, and STEM education programs from Ahmedabad.

CubeSat Aerospace

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	100mm × 100mm × 113.5mm
Weight	~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

price on request

CubeSat Aerospace

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

price on request

CubeSat Aerospace

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	Custom slots for trays, fasteners, and tools

price on request

Vertically integrated Indian defence and aerospace electronics company designing and manufacturing avionics, microelectronics, RF/microwave, radar, test equipment and space systems.

Data Patterns (India) Ltd.

Gimbal and Actuator Controller Products

BLDC motor drivers and actuator controllers for gimbal, thrust vector and control surfaces

price on request

German manufacturer of space deployables using patented Shape Memory and Origami technologies — release actuators, solar arrays, and antenna deployables for CubeSats and microsatellites.

Dcubed

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

price on request

Dcubed

Release Nuts

A family of release nuts designed for various space applications, offering different sizes, masses, and axial load capacities.

Size (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
Size (Nano Release Nut nD3RN)	17x17x17 mm / 0.67x0.67x0.67 in

price on request

DeltaV Robotics was founded by Niha Agarwalla and Naushad Rahman, who have experience in commercial and defense space, including flight-proven spacecraft engineering.

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.

Deployable Space Systems (DSS) — now Redwire

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.

SIZE (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

price on requestdatasheet

Developer of fluid-dynamic attitude control systems, gyroscopes, and air bearings for the space industry.

ElmSpace

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

price on request

Software-flexible CubeSat platforms (1U–16U+), shared-satellite hosted-payload service.

EnduroSat

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

price on request

EnduroSat

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

price on request

US manufacturer of non-explosive actuators (TiNi FrangiBolt, pin pullers, ejectors) and energetic hold-down and release systems.

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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 50ms
RESISTANCE	0.95 to 1.6Ω @ 23°C

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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,

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on requestdatasheet

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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)

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

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

price on request

Berlin-based launch and deployment services company providing end-to-end rideshare missions, satellite integration, and proprietary separation hardware for small satellites.

Exolaunch

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

price on requestdatasheet

Exolaunch

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

price on requestdatasheet

Developer of multimode chemical-electric propulsion systems for small satellites.

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 market.

Frond Space Systems

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)

price on request

Gama Space develops solar sail propulsion for low-cost deep space missions and Astrobrake, an autonomous drag sail for satellite deorbiting compliance.

Gama Space

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

price on request

GITAI develops robotic technologies for space exploration, including solutions for satellite construction, lunar settlements, and Martian cities, with a robot currently on the ISS.

GITAI

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)

price on request

Glavkosmos coordinates international human spaceflight projects, facilitates satellite launches, develops and supplies rocket components, and provides equipment for space crews.

Glavkosmos

Antenna Reflector Hold-down Lock (mechanical) Type 1

A mechanical hold-down lock designed to secure antenna reflectors in the stowed position on spacecraft.

Year of release	2011
Guaranteed service life (years)	6
Estimated production / delivery time (months)	4
Clamping force, kg	600
Ultimate bending moment at the interface surface with the spacecraft, N·m	200

price on request

Glavkosmos

Antenna Reflector Hold-down Lock (mechanical) Type 2

A mechanical hold-down lock designed to secure antenna reflectors in their stowed position during launch and orbital maneuvers, featuring a clamping force of 400 kg.

Purpose	Holding antenna reflector in the stowed position.
Year of release	2016
Guaranteed service life (years)	6
Estimated production / delivery time (months)	4
Clamping force, kg	400

price on request

Glavkosmos

Conical Adapter. Type 1

The Conical Adapter Type 1 provides a specified interface between a spacecraft and an upper stage, featuring a conical grid shell made from CFRP with two interface rings.

Purpose	Providing specified interface between the spacecraft and upper stage.
Flight qualification of the product	Yes
Brief history of flight qualification	Flight qualification since 2000.
Possibility to adapt the product to customer requirements	Yes
Height, mm	650

price on request

Glavkosmos

Conical Adapter. Type 2

The Conical Adapter Type 2 is a flight-qualified CFRP conical grid shell designed to provide a specified interface between a spacecraft and an upper stage, such as the Fregat-SB bo

Purpose	Providing specified interface between the spacecraft and upper stage.
Flight qualification of the product	Yes
Brief history of flight qualification	Flight qualification since 2000.
Possibility to adapt the product to customer requirements	Yes
Height, mm	398.5

price on request

Glavkosmos

Conical Adapter. Type 3

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

Height	1200 / 150 / 900 / 150 mm (4 configurations)
Mass	134.82 / 19.82 / 115 / 115 kg (4 configurations)
Ring bore diameter (upper-lower joint)	1172-2040 / 1172-1294 / 1294-2000 / 2000-2040 mm
Compatible launch vehicle	Persei (14S48) booster / Angara launch vehicle
Flight heritage	Flight-qualified since 2000

price on request

Glavkosmos

Conical Adapter. Type 4

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

Height	650 mm
Mass	62 kg
Ring bore diameter (upper-lower joint)	1172-2040 mm
Compatible launch vehicle	Persei (14S48) booster / Angara launch vehicle
Flight heritage	Flight-qualified since 2000

price on request

Glavkosmos

Conical Adapter. Type 5

Conical grid-shell adapter providing the mechanical interface between a spacecraft and its upper stage.

Height	900 mm
Mass	91.14 kg
Ring bore diameter (upper-lower joint)	1172-2040 mm
Compatible launch vehicle	Persei (14S48) booster / Angara launch vehicle
Flight heritage	Flight-qualified since 2000

price on request

Glavkosmos

Deployment Mechanism of Large Flat Antenna

This is a deployment mechanism designed for large flat antennas, intended for use as a component within larger antenna systems on spacecraft.

Purpose	Component of large antenna systems.
Flight qualification of the product	No
Possibility to adapt the product to customer requirements	Yes
Aperture	3m×100m
Deployment mechanism mass	≤1200 kg

price on request

Glavkosmos

Glazing of Spacecraft

Heat-resistant, high-strength, radiation-optically-resistant glass of optical quality designed for spacecraft cockpit glazing, capable of withstanding pressure differences and extr

Year of release	1979
Guaranteed service life (years)	at least 15 years
Estimated production / delivery time (months)	2-3
Flight qualification of the product	Yes
Brief history of flight qualification	Buran spacecraft.

price on request

Glavkosmos

Harmonic Drive. Type 1

The Harmonic Drive Type 1 is a high-precision gear drive designed for antenna pointing applications, offering a guaranteed service life of 15 years.

Purpose	Used as part of high-precision antenna pointing drive.
Year of release	2014
Guaranteed service life	15 years
Estimated production / delivery time	2 months
Transfer error, arcsec, not exceeding	±40

price on request

Glavkosmos

Harmonic Drive. Type 2

The Harmonic Drive Type 2 is a high-precision gear drive designed for use in antenna pointing mechanisms, offering high accuracy and a long operational life.

Purpose	Used as part of high-precision antenna pointing drive.
Year of release	2014
Guaranteed service life	15 years
Estimated production / delivery time	2 months
Transfer error, arcsec, not exceeding	±30

price on request

Glavkosmos

Honeycomb Panel with Composite Face Sheets

Honeycomb panels with composite face sheets designed for distributing high-precision and dimensionally stable equipment, offering customization and integration options for thermal

Purpose	Distribution of high-precision and dimensionally stable equipment.
Flight qualification of the product	Yes
Brief history of flight qualification	Flight qualification since 2000.
Possibility to adapt the product to customer requirements	Yes
Maximum dimensions, mm	5800kh3000

price on request

Glavkosmos

Linear Drive

The Linear Drive is a high-precision electromechanical linear positioning drive designed for synchronizing force spoke motion or transfer during antenna deployment.

Axial travel rate, mm/s	0.4 - 0.8
Axial shear force, N	2000
Supply voltage, V	27
Consumption current of two electric motors, A, not exceeding	0.4
Operating temperature range, °C	-50 to +70

price on request

Glavkosmos

Load-bearing Structure of the Enclosure. Type 1-A

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Angle between intersection nodes of spiral fins	6°
Angle between two spiral fins	28°
Spiral fins thickness	6+1 mm
Circumferential fins thickness	2+1 mm
Distance between intersection nodes of spiral fins	144 mm

price on request

Glavkosmos

Load-bearing Structure of the Enclosure. Type 1-B

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Angle between intersection nodes of spiral fins	6°
Angle between two spiral fins	28°
Spiral fins thickness	6+1 mm
Circumferential fins thickness	2+1 mm
Distance between intersection nodes of spiral fins	144 mm

price on request

Glavkosmos

Load-bearing Structure of the Enclosure. Type 2

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Angle between intersection nodes of spiral fins	7.5°
Angle between two spiral fins	42°
Spiral fins thickness	10±1 mm
Circumferential fins thickness	4±1 mm
Longitudinal fins thickness	10±1 mm

price on request

Glavkosmos

Load-bearing Structure of the Enclosure. Type 3

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Angle between intersection nodes of spiral fins	7.5°
Angle between two spiral fins	58.9°
Spiral fins thickness	3±1 mm
Circumferential fins thickness	3±1 mm
Longitudinal fins thickness	4.2±1 mm

price on request

Glavkosmos

Load-bearing Structure of the Enclosure. Type 4

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Angle between intersection nodes of spiral fins	7.5°
Angle between two spiral fins	42°
Spiral fins thickness	4.5±1 mm
Circumferential fins thickness	3±2 mm
Longitudinal fins thickness	6±1 mm

price on request

Glavkosmos

Load-bearing Structure of the Enclosure. Type 5

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Angle between intersection nodes of spiral fins	7.5°
Angle between two spiral fins	59.5°
Spiral fins thickness	3±1 mm
Circumferential fins thickness	3±3 mm
Longitudinal fins thickness	4.2±1 mm

price on request

Glavkosmos

Load-bearing Structure of the Enclosure. Type 6

Cylindrical CFRP grid-shell load-bearing structure for mounting spacecraft subsystems and equipment.

Angle between intersection nodes of spiral fins	7.5°
Angle between two spiral fins	73°2'
Spiral fins thickness	6±0.5 mm
Circumferential fins thickness	3±0.5 mm
Distance between intersection nodes of spiral fins	152.88 mm

price on request

Glavkosmos

Mechanical Device Hold-down Lock (mechanical, involving release device)

A mechanical hold-down and release device designed to secure deployable elements of a mechanical device in a stowed position during launch and then release them in orbit.

Year of release	2016
Guaranteed service life	6 years
Flight qualification of the product	o
Possibility to adapt the product to customer requirements	Yes
Clamping force	1000 kg

price on request

Glavkosmos

Mechanical Unit of Antenna Pointing System. Type 2

A two-degree-of-freedom electromechanical drive unit that rotates a satellite antenna mounting plane relative to the antenna pointing system control module in two mutually perpendi

Estimated production / delivery time	6 months
Rotation angle for each axis	± 25 °
Slew rate	0.009-7.1 °/min
Measurement error of the rotation angle for each axis, not exceeding	90 arcsec
Developed torque for each axis, not less than	30 N·m

price on request

Glavkosmos

Mechanical Unit of Antenna Pointing System. Type 3

A two-degree-of-freedom electromechanical drive designed for antenna pointing, providing rotation of an antenna's mounting plane in two mutually perpendicular axes.

Rotation angle for each axis, °	± 10; ± 90
Slew rate, °/min	0.009- 7.2
Measurement error of the rotation angle for each axis, arcsec, not exceeding	90
Developed torque for each axis, N·m, not less than	60
Load inertia moment, kg·m2, not exceeding	160

price on request

Glavkosmos

Mechanical Unit of Antenna Pointing System. Type 4

A two-degree-of-freedom electromechanical drive designed to provide precise rotation for spacecraft antennas in two mutually perpendicular planes.

Year of release	2014
Guaranteed service life (years)	15
Estimated production / delivery time (months)	6
Rotation angle for each axis	±16 °
Slew rate	0-7 °/min

price on request

Glavkosmos

Multi-layer Composite Structures

Multi-layer composite structures designed for thermal control and as strength elements of spacecraft, featuring aluminum and carbon fiber skins with aluminum foil honeycombs.

Purpose	Thermal control of spacecraft equipment. Strength elements of spacecraft bodies.
Year of release	1998
Guaranteed service life (years)	20 years
Estimated production / delivery time (months)	3
Flight qualification of the product	Yes

price on request

Glavkosmos

Multi-Layer Honeycomb Panel

Multi-layer honeycomb panels designed for distributing high-precision and dimensionally stable equipment, available with fixed or attachable heat transfer tubes or fluid loops.

Purpose	Distribution of high-precision and dimensionally stable equipment.
Flight qualification of the product	Yes
Brief history of flight qualification	Flight qualification since 2000.
Possibility to adapt the product to customer requirements	Yes
Honeycomb filler sort	Amg2N, Amg5N (rus)

price on request

Glavkosmos

Propulsion Thruster Drive Mechanism

A one-degree-of-freedom electromechanical device that rotates a three-thruster propulsion unit around a single axis, holds it in transport position during launch, and regulates its

Purpose	Rotation of the unit consisting of three propulsion thrusters around one axis within the s
Year of release	2003
Guaranteed service life (years)	15
Estimated production / delivery time (months)	4
Rotation angles of the engine installation surfaces, °	±10.5

price on request

Glavkosmos

Reflector Drive Mechanism

The Reflector Drive Mechanism is a two-degree-of-freedom electromechanical device designed to rotate a large deployable antenna reflector on a spacecraft from its transportation to

Guaranteed service life	10 years
Estimated production / delivery time	6 months
Readjustment/rotation angle for each axis	up to ± 25 °
Rotation angle to the operating position	up to 290 °
Slew rate	0.009-7.0 °/min

price on request

Glavkosmos

Reflector form Readjustment Device

An electromechanical device utilizing linear drives to precisely adjust the operating surface profile of large reflectors based on control system commands.

Number of thrusts, units	8 or 12
Thrust force, N	260
Working path, mm	± 20
Thrust transfer error, mm, not exceeding	0.125
Thrust transfer rate, mm/min	0.7 - 1

price on request

Glavkosmos

Reflector Transfer Mechanism

The Reflector Transfer Mechanism is a two-degree-of-freedom electromechanical device for deploying and pointing antenna reflectors on spacecraft.

Purpose	Antenna deployment and alignment.
Year of release	2013
Guaranteed service life (years)	10
Estimated production / delivery time (months)	6
Readjustment/rotation angle for each axis	±90 °

price on request

Glavkosmos

Release Device (electromechanical, shock-free). Type 1

The Release Device (electromechanical, shock-free) Type 1 is designed to hold mechanical device hold-down locks in a cocked position, ensuring secure retention until release is req

Year of release	2015
Guaranteed service life	8 years
Estimated production / delivery time	4 months
Brief history of flight qualification	2019
Rod load	6 kg

price on request

Glavkosmos

Retractable Mast Mechanism

A linear electromechanical mechanism designed for the deployment and fixation of umbrella-type deployable reflectors on spacecraft.

Purpose	Deployment of the reflector from the transportation to the operational position and its fi
Year of release	2005
Guaranteed service life (years)	10
Estimated production / delivery time (months)	6
Mast retraction time, min	30

price on request

Glavkosmos

Shaping Telescopic Element in the Construction of a Large-sized Transformable Reflector

A shaping telescopic element designed for the deployment of large transformable reflectors on geostationary spacecraft, allowing for the disclosure of multi-pointed spokes with rev

Purpose	Disclosure of elements of a large transformable reflector to work on spacecraft in geostat
Year of release	2015
Guaranteed service life	17 years
Estimated production / delivery time	12 months
Possibility to adapt the product to customer requirements	Yes

price on request

Glavkosmos

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
Guaranteed service life	6 years
Estimated production / delivery time	2 months
Flight qualification of the product	No

price on request

Glavkosmos

Single-actuation Drive. Type 1

The Single-actuation Drive Type 1 is an electromechanical rotary drive designed for the deployment of spacecraft structure elements such as solar array panels, booms, and antennas.

Purpose	Deployment of spacecraft structure elements: solar array panels, booms, antennas.
Year of release	2009
Estimated production / delivery time (months)	6
Brief history of flight qualification	Amos-5, Telkom-3, KazSat-3, Express-AT1, Express-AT2, Express-AM8.
Nominal slew rate	2 – 4 °/s

price on request

Glavkosmos

Single-actuation Drive. Type 2

The Single-actuation Drive Type 2 is an electromechanical rotary drive designed for the deployment of spacecraft structure elements such as solar array panels, booms, and antennas.

Purpose	Deployment of spacecraft structure elements: solar array panels, booms, antennas.
Year of release	2006
Estimated production / delivery time	6 months
Brief history of flight qualification	Express-AM, Spektr-R, Elektro-L.
Nominal slew rate	1-3 °/s

price on request

Glavkosmos

Single-actuation Drive. Type 3

The Single-actuation Drive, Type 3, is an electromechanical rotary drive designed for the deployment of large mechanical system elements on spacecraft, such as solar array panels,

Year of release	2012
Estimated production / delivery time (months)	6
Brief history of flight qualification	Express-AM5, Express-AM6,Yamal-401
Nominal slew rate, °/s	1.2-2.8
Torque rating, N·m	25

price on request

Glavkosmos

Single-actuation Drive. Type 4

The Single-actuation Drive Type 4 is an electromechanical rotary drive designed for the deployment of spacecraft structural elements such as solar array panels, booms, and antennas

Year of release	2005
Estimated production / delivery time	6 months
Brief history of flight qualification	Loutch-5A, Loutch-5B, Loutch-5V
Nominal slew rate	0.3 - 0.7 °/s
Torque rating	60 N·m

price on request

Glavkosmos

Single-Actuation Drive. Type 5

The Single-Actuation Drive, Type 5, is an electromechanical rotary drive designed for the deployment of large mechanical system elements on spacecraft, such as solar arrays, booms,

Purpose	Deployment of spacecraft structure elements: solar array panels, booms, antennas.
Year of release	2010
Estimated production / delivery time (months)	12
Brief history of flight qualification	No
Nominal slew rate	2 °/s

price on request

Glavkosmos

Single-Actuation Drive. Type 6

The Single-Actuation Drive Type 6 is an electromechanical rotary drive designed for the deployment of large mechanical system elements on spacecraft, including solar array panels,

Year of release	2010
Estimated production / delivery time	12 months
Brief history of flight qualification	No
Nominal slew rate	0.25; 1 °/s
Torque rating	0-110 N·m

price on request

Glavkosmos

Solar Array Drive Mechanism. Type 1

Flight-proven SADM (5.3 kg, 280 A power transfer, 25 power circuits, 140,000-hr life). Heritage: Express-AM5, Express-AM6.

Purpose	Solar array wing rotation, power transmission, telemetry signal routing, shaft angle measu
Year of release	2010
Guaranteed service life, years	15.25
Estimated production/delivery time	12 months
Flight heritage	Express-AM5, Express-AM6

price on request

Glavkosmos

Solar Array Drive Mechanism. Type 2

The Solar Array Drive Mechanism (SADM) Type 2 is an electromechanical device designed for the precise rotation of solar array wings on spacecraft, ensuring optimal power generation

Purpose	Rotation of solar array wings at the specified rate; electrical power transmission from ro
Year of release	2013
Guaranteed service life (years)	13.5
Estimated production / delivery time (months)	15
Flight qualification of the product	yes

price on request

Glavkosmos

Solar Array Drive Mechanism. Type 3

An electromechanical solar array drive mechanism designed for continuous rotation of solar array wings, electrical power transmission, and output shaft rotation angle signal genera

Purpose	Rotation of solar array wings at the specified rate; electrical power transmission for con
Year of release	1995
Guaranteed service life (years)	7
Estimated production / delivery time (months)	12
Flight qualification of the product	Yes

price on request

Glavkosmos

Solar Array Drive Mechanism. Type 5

The Solar Array Drive Mechanism (SADM) Type 5 is an electromechanical device designed for the continuous rotation of solar array wings on spacecraft, ensuring optimal power generat

Year of release	2006
Guaranteed service life (years)	10
Estimated production / delivery time (months)	12
Flight qualification of the product	Yes
Brief history of flight qualification	Glonass-K.

price on request

Glavkosmos

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
Guaranteed service life (years)	3
Estimated production / delivery time (months)	2
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.).

price on request

Glavkosmos

Two-degree-of-freedom Antenna Pointing Device. Type 1

The Two-degree-of-freedom Antenna Pointing Device. Type 1 is an electromechanical system designed for precise pointing of spacecraft antennas towards mobile and immobile users.

Purpose	Spacecraft antennas pointing to mobile and immobile users.
Year of release	2007
Guaranteed service life (years)	10
Estimated production / delivery time (months)	6
Flight qualification of the product	No

price on request

Glavkosmos

Two-degree-of-freedom Device for Antenna Pointing. Type 2

This is a two-degree-of-freedom electromechanical device designed for precise antenna pointing on spacecraft, enabling communication with both mobile and immobile users.

Year of release	1985
Guaranteed service life	5 years
Estimated production / delivery time	6 months
Flight qualification of the product	Yes
Rotation angle for each axis	± 11.5 °

price on request

Glavkosmos

Two-degree-of-freedom Device for Antenna Pointing. Type 3

An electromechanical two-degree-of-freedom device designed for precise pointing of spacecraft antennas towards both mobile and immobile users.

Purpose	Spacecraft antennas pointing to mobile and immobile users.
Year of release	1988
Guaranteed service life	5 years
Estimated production / delivery time	6 months
Flight qualification of the product	Yes

price on request

Glavkosmos

Two-degree-of-freedom device for antenna pointing. Type 4

An electromechanical device designed for precise antenna pointing on spacecraft, offering two degrees of freedom for tracking mobile and immobile users.

Year of release	1996
Guaranteed service life (years)	10
Estimated production / delivery time (months)	6
Flight qualification of the product	Yes
Rotation angle for each axis	± 10.5 °

price on request

System integrator and manufacturer of CubeSat structures, buses, and MyPOD test/transport pods, with space environment test equipment services.

Gran Systems

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 113.5mm
Max. PC105 PCB Size	95.9 x 95.9 mm
Average weight	118 g
Material	Aluminum T6 6061

price on request

Gran Systems

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 340mm
Max. PC105 PCB Size	95.9 x 95.9 mm
Deployable Dimensions	L 104 × W 104 × H 340mm
Average weight	580 g

price on request

Gran Systems

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 366mm
Deployable Dimensions	L 104 × W 230.3 × H 366mm
Average weight	916 g
Material	Aluminum T6 6061

price on request

HPS designs, manufactures, and integrates mechanical/thermal space subsystems, including antennas, deployable structures, thermal insulation, and equipment for nanosatellites.

HPS High Performance Space Structure Systems

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

price on request

CubeSat deployers, antennas, EPS and small-satellite systems.

ISISPACE Group

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

price on request

ISISPACE Group

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

price on request

Russian satellite manufacturer in Zheleznogorsk, Siberia; GLONASS-K/M navigation, Express GEO comms, Luch data relay, and Yamal satellites; 1,400+ spacecraft built.

ISS Reshetnev

Antenna Deployment and Pointing Mechanisms

ISS Reshetnev designs and manufactures a broad family of Antenna Deployment and Pointing Mechanisms (ADPM) and Reflector Deployment and Pointing Mechanisms (RDPM) for spacecraft. T

price on request

South Korean nanosatellite manufacturer offering CubeSat platforms, optical imagers, star trackers, solar panels, EPS, structures, and deployers for the commercial small satellite market.

Kairo Space

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

price on request

Kall Morris Inc provides in-space logistics, scavenging, and long-haul transport solutions, developing spacecraft and systems for satellite mobility and orbital debris management.

Kall Morris Inc

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

price on requestdatasheet

Kayser Space designs, manufactures, integrates, and tests hardware and platforms for space programs, supporting over 100 missions and microgravity research.

Kayser Space

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.

price on request

CubeSat & small-satellite rideshare brokerage — integration, paperwork, launch insurance on PSLV, Falcon 9 Transporter, Ariane 6 and Soyuz.

KOSMOLAB Launch Services

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, mm	≥ 4.5
Pull force, kg	0.45 ± 0.05 kg
Operating temperature, °C	-60°C to +60°C

price on requestdatasheet

USA 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.

KSF Space Foundation

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)

$1 000

L.Garde designs, develops, and manufactures inflatable and deployable structures for space and terrestrial applications, including solar sails and advanced observation structures.

L.Garde Inc

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

price on request

Polish manufacturer of small satellites, CubeSat components, and subsystems for Earth observation and communications missions.

Lamb Space Tec

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
Lifetime	>500,000 cycles
Temperature range	-20°C to +70°C (extendable)

price on request

Large Space Structures GmbH designs and manufactures large deployable reflector technologies for space applications, including LDRs and deployable antennas.

Large Space Structures GmbH

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

price on request

Materion designs and manufactures advanced materials, including specialty alloys, chemicals, metals, beryllium composites, and optical coatings, for various industries including aerospace and defense.

MDA Space designs and manufactures robotics, satellite systems, and provides geointelligence services for the global defense and space industry.

MDA Space

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)

price on request

Memetis GmbH designs and manufactures ultracompact microvalves and highly integrated microfluidic systems for space, life science, and medical technology applications.

Memetis

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

price on request

Memetis

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

price on request

Memetis

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

price on request

Micromotion GmbH designs and manufactures high-precision micro drive technology, including micro drives and micro gearboxes, for various applications including space technology.

Micromotion GmbH

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

price on request

Micromotion GmbH

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

price on request

Micromotion GmbH

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

price on request

Chinese commercial satellite manufacturer building Earth observation, communications, and remote sensing satellites, plus payloads, components, and ground terminal systems.

MinoSpace

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 2Hz

price on request

MinoSpace

Damper

A fully mechanical damper designed for controlled slow deployment of passive mechanisms in space applications.

price on request

MMA Design manufactures deployable solutions for space and terrestrial missions, including de-orbit systems and solar arrays, and is headquartered in Broomfield, Colorado.

MMA Design

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

price on request

MMA Design

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

price on request

Precision motion control and propulsion systems provider for space and defense applications.

Moog Space Defense Group

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

price on request

Motiv Space Systems designs and builds space robotics, motor controllers, and mechanisms, including the robotic arm on NASA's Mars 2020 Perseverance rover.

Motiv Space Systems

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

price on requestdatasheet

Motiv Space Systems

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	3D Images
Mastcam-Z Key Capabilities	Panoramic Color Imaging
Mastcam-Z Key Capabilities	28-100mm Zoom Range
Mastcam-Z Key Capabilities	Ability to Resolve Features 1mm Across at a Distance of 100-Meters

price on request

Motiv Space Systems

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	45kg (Earth gravity)
Kinematics	5-DOF
Reach	2.1 meters
Environment	-135°C; Martian Dust and Radiation Hardened
Accuracy	<1 millimeter

price on request

Motiv Space Systems

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.

price on request

Motiv Space Systems

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

price on requestdatasheet

German aerospace components manufacturer producing satellite tanks, CFRP structures, and antenna dishes for European satellite programs.

MT Aerospace

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

price on request

Pre-integrated nanosatellite buses (3U–16U+ MP42), green chemical propulsion, mission integration.

NanoAvionics

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

€5 040

Uzbekistan's first private aerospace engineering research and development center, building rocket prototypes, modular satellite platforms, and running national space-education programs.

Polish smallsat hardware company designing and manufacturing components and subsystems for CubeSats and small satellites, serving commercial and institutional space customers across Europe.

Needronix

Satellite Transport Boxes

Custom foam-lined transport and shipping containers for CubeSats and small satellites — vibration isolation, ESD protection, humidity control, ISSTA and MIL-SPEC-grade protective p

Protection	Vibration-isolating foam, ESD shielding, humidity control
Standards	MIL-SPEC, ISSTA protective packaging
Configurations	Full satellite, subsystem, and component variants

price on request

Nimesis Technology designs and manufactures space actuators and mechanisms using shape memory alloys for satellites, launchers, and other space applications.

Nimesis Technology

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

price on request

Nimesis Technology

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

price on request

Minotaur family, Pegasus XL, Antares (legacy); MLV co-development with Firefly.

Northrop Grumman Space Systems

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

price on requestdatasheet

NPC Spacemind designs and manufactures CubeSat separation systems, deployers, and subsystems, including deorbiting systems, for nanosatellites and CubeSats.

NPC Spacemind

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

price on request

NPC Spacemind

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

price on request

NPC Spacemind

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

price on request

NPC Spacemind

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

price on request

NPC Spacemind

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

price on request

NPC Spacemind

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

price on request

NPC Spacemind

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

price on request

NPC Spacemind

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

price on requestdatasheet

NPC Spacemind

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

price on request

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.

Opterus Research and Development

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

price on requestdatasheet

Opterus Research and Development

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.

price on requestdatasheet

Robotic additive manufacturing company producing high-performance composite parts for aerospace, defense and space applications at scale.

Orbital Composites

Orbital S Multi-Robot 3D Printer

Flagship multi-robot, multi-material 3D printing platform for tooling-free composite part production.

price on request

Orbital Composites

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

price on request

In-space manufacturing company building 3D-printing hardware that constructs large structural booms and infrastructure directly in orbit.

Orbital Matter

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

price on request

Orbotic 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

Orbotic Systems

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

price on request

PacSci EMC designs and manufactures mission-critical pyrotechnic and energetic material devices and integrated systems for aerospace, defense, energy and space applications.

PacSci EMC

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

price on request

PacSci EMC

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	TLX or SMDC input
Input Stimulus, Typical	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

price on requestdatasheet

Polish robotics and space technology company developing robotic systems, space mechanisms, and rover technologies for planetary exploration and satellite servicing missions.

PIAP Space

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

price on request

PIAP Space

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

price on request

Plan-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)

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

price on request

Advanced 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.

Princeton Satellite Systems

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.

Weight	0.350 kg
Dimensions	10 × 10 × 10 cm

price on request

Spanish composites engineering company designing and manufacturing deployable carbon-fiber structures, antennas and instruments for space, aerospace, marine defense and marine racing applications.

Prosix Engineering

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	Utracompact
SPACE DEPLOYABLE MASTS - Characteristics	High stiffness, accuracy and stability
SPACE DEPLOYABLE MASTS - Characteristics	Modular, Scalable

price on request

Prosix Engineering

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

price on request

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 successful space missions since 2003.

Pumpkin, Inc.

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

$110

Pumpkin, Inc.

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

$88

Pumpkin, Inc.

3U CubeSat Display Model

A full-size (340.5mm x 100mm x 100mm) plastic display model of a 3U CubeSat following the CubeSat Design Specification, reproducing Pumpkin's CubeSat Kit structures with realistic

Dimensions	340.5 mm x 100 mm x 100 mm
Form factor	3U CubeSat (per CubeSat Design Specification)
Construction	One-piece plastic model, not intended to be disassembled
Solar panels	Dummy solar panels with realistic solar cell stickers on all six faces
Classification	Display Hardware, Not for Flight

$1 500datasheet

Pumpkin, Inc.

6U CubeSat Display Model

A full-size (approximately 360.5mm x 200mm x 100mm) plastic display model of a 6U tabbed CubeSat compatible with the Rocket Lab CSD 6U deployer, reproducing Pumpkin's SUPERNOVA 6U

Dimensions	approximately 360.5 mm x 200 mm x 100 mm
Form factor	6U tabbed CubeSat
Compatible dispensers	Rocket Lab CSD 6U, Maverick Space Systems (MSS) Mercury-6, and similar
Solar array simulation	64-cell 'propeller' configuration, deployed, on four panels, detachable
Classification	Display Hardware, Not for Flight

$3 000datasheet

Pumpkin, Inc.

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

$1 610datasheet

Pumpkin, Inc.

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

$865datasheet

Pumpkin, Inc.

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

$690 – $1 560

Pumpkin, Inc.

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

$1 085

Pumpkin, Inc.

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	97mm x 97mm
Construction	One-piece

$1 215 – $2 955datasheet

Pumpkin, Inc.

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

$495datasheet

Pumpkin, Inc.

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

$955 – $1 085datasheet

Pumpkin, Inc.

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

$820

Pumpkin, Inc.

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)

$690 – $820datasheet

Pumpkin, Inc.

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

$360

Pumpkin, Inc.

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

$495datasheet

Pumpkin, Inc.

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

$22 500 – $39 500

Pumpkin, Inc.

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

$200datasheet

Pumpkin, Inc.

Pelican Ruggedized Transport Case

A ruggedized Pelican-brand transport/storage case sold by Pumpkin as an accessory for safely transporting CubeSat Kit hardware.

SKU	632-00372
Price	$265.00 per item

$265

Pumpkin, Inc.

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

$165datasheet

Pumpkin, Inc.

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

$70datasheet

Pumpkin, Inc.

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.

price on requestdatasheet

Pumpkin, Inc.

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	0.062"/1.6 mm

$395datasheet

Redwire 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 (Redwire)

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

price on request

Swiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.

RUAG Space

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

price on requestdatasheet

RUAG Space

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

price on requestdatasheet

RUAG Space

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

price on request

RUAG Space

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)

price on requestdatasheet

RUAG Space

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

price on requestdatasheet

RUAG Space

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

price on request

RUAG Space

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

price on requestdatasheet

RUAG Space

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

price on requestdatasheet

RUAG Space

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

price on requestdatasheet

RUAG Space

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

price on request

RUAG Space

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

price on request

Spanish engineering company supplying precision mechanisms, solar array drive assemblies, and structural components for ESA and commercial satellite missions.

SENER Aeroespacial

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

price on request

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.

Serenum Space

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

price on request

Chinese developer and manufacturer of small solid rockets, weather-modification rocket systems, sounding rockets, guided rockets, and advanced aerospace materials.

Shaanxi Zhongtian Rocket Technology Co., Ltd.

Static Space Model

Large-scale customizable indoor/outdoor rocket and spacecraft static display models for aerospace science education and exhibitions.

Type	Static (non-flying) display model
Scale	Customizable per customer requirement
Application	Indoor/outdoor display; aerospace science education, expo, exhibitions
Design standard	Aerospace Military Standard
Customization	Large-scale static simulation custom orders accepted

price on request

Sheldahl (Multek Flexible Circuits) is a US manufacturer of flexible printed circuits, printed electronics, electronic materials, and aerospace thermal control materials, headquartered in Northfield, Minnesota.

Sheldahl (Multek Flexible Circuits)

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

price on request

Sheldahl (Multek Flexible Circuits)

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

price on request

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 from its Florida Space Coast facilities.

Sidus Space, Inc.

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

price on requestdatasheet

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.

Sierra Space

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

price on requestdatasheet

Sierra Space

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

price on request

Sierra Space

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

price on request

Sierra Space

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

price on request

Sierra Space

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

price on requestdatasheet

Sierra Space

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

price on request

Skycorp designs the Orbital Logistics Vehicle, a reusable, on-orbit-assembled space platform with a standardized interface for hosting modular third-party payloads.

Skycorp Incorporated

Intelligent Space Systems Interface (iSSI)

Standard, robotic on-orbit connector/bus interface providing power, data, bandwidth and physical rigidity for modular payload integration.

price on request

Skycorp Incorporated

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

price on requestdatasheet

Belgian engineering company delivering systems, products, and services for manned and unmanned spaceflight, robotics, mission control, and astronaut training.

Space Applications Services

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

price on requestdatasheet

UK company (Cardiff, Wales) developing reusable in-space manufacturing platforms and a non-ablative reentry heat shield for producing semiconductor materials in microgravity.

Space Forge Limited

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)

price on request

German company (Berlin) providing structural engineering, analysis, and manufacturing of mechanical subsystems for spacecraft, including struts, sandwich panels, precision assemblies, and bolt/vibration analysis software.

Space Structures GmbH

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

price on request

Space Structures GmbH

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

price on request

Space Structures GmbH

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,

price on request

Swiss innovation and research center specializing in microelectronics, photonics, and digital technologies, with significant contributions to space and satellite instrumentation.

Swiss Centre for Electronics and Microtechnology (CSEM)

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

price on requestdatasheet