Space Hardware Marketplace

SCR-106 / SCR-106HDR X-Band Software-defined Compact Radio

X-band software-defined radio with up to 20 Mbps downlink (SCR-106) or 100 Mbps (SCR-106HDR), on-orbit configurable, flight heritage…

SCR-104 S-Band Software-defined Compact Radio

On-orbit configurable S-band software-defined radio for CubeSat and SmallSat, 4.5+ Mbps downlink, USB and AFSCN SGLS support, flight…

SARA21 General Purpose Rotary Actuator

• Units in spaceMore than 110; first flight 2005
• Production capacityUp to 50 units per year; in continuous production for 20 years
• InterfaceSimple stepper motor interface

Compact, back-drivable general purpose rotary actuator with more than 110 units in space since 2005 and a simple…

SEPTA42 Solar Array Drive Mechanism

• Target applicationSmall satellites and constellations
• Production rateUp to 18 units per month
• Units deliveredMore than 100 flight models

Constellation SADM for small satellites, produced at up to 18 units per month with more than 100 flight…

SEPTA36G Solar Array Drive Mechanism

• TypeSolar Array Drive Mechanism (high power class, demanding missions)
• QualificationFully qualified; qualified for LEO and GEO missions
• Slip ringFlight proven in-house slip ring technology

Fully qualified Solar Array Drive Mechanism variant of the modular SEPTA family for demanding missions.

SEPTA36 Solar Array Drive Mechanism

• TypeSolar Array Drive Mechanism (high power class)
• QualificationFully qualified; qualified for LEO and GEO missions
• Slip ringIn-house gold-on-gold slip ring technology

Fully qualified high-power Solar Array Drive Mechanism from Beyond Gravity's modular SADM family, qualified for LEO and GEO…

Separation Nut PSM 1/2B

• Target spacecraft classConstellation class satellites, typically 500-1000 kg
• QualificationAIAA S-113-2005 (former DOD-E-83578A)
• InitiatorsDual NSI equivalent (PC23, 103377-191/-449/-500, PD222400024-009, 2-8001140-1, 852420-XX)

Low-shock separation nut for constellation-class satellites of typically 500-1000 kg, qualified per AIAA S-113-2005.

Separation Nut PSM 3/8B

• Target spacecraft classOneWeb class satellites, typically 100-200 kg
• QualificationAIAA S-113-2005 (former DOD-E-83578A)
• InitiatorsDual NSI equivalent (PC23, 103377-191/-449/-500, PD222400024-009, 2-8001140-1, 852420-XX)

Smallest low-shock separation nut of the family, developed to fit OneWeb-class satellites of typically 100-200 kg.

PAS 432S (17 in) Separation System

• Interface diameter432 mm (17 in)
• First applicationSatellites up to 200 kg at 0.45 mm on the VEGA launch vehicle
• Release mechanismCBOD-LT Separation System Release Mechanism

Low-shock clamp band separation system designed for satellites up to 200 kg at 0.45 mm on the VEGA…

PAS 610S (24 in) Separation System

• Interface diameter610 mm (24 in)
• CompatibilityMoog CSA ESPA; ESPA Rideshare User's Guide environments
• Release mechanismCBOD-LT Separation System Release Mechanism

Low-shock separation system whose load capability is fully compatible with the Moog CSA ESPA and the ESPA Rideshare…

ESPA Separation System (PSR 1575 mm / 62 in)

• Interface diameter1575 mm (62 in)
• CompatibilityEELV Secondary Payload Adapter (ESPA)
• Release mechanismCBOD Low Shock Release Mechanism

1575 mm (62 in) low-shock clamp band separation system fully compatible with the EELV Secondary Payload Adapter (ESPA).

PAS 381S (15 in) Separation System

• InterfaceESPA 15 in adapter interface
• Release mechanismCBOD-LT Separation System Release Mechanism
• Scope of supplyLow shock clamp band separation system, interface rings, umbilical connection, separation spring set

Smallest member of the low-shock separation system family, developed to fit the ESPA 15 inch adapter interface.

ARROW 450 Satellite Bus

• Position in familyLarger and more modular than the ARROW150
• Design basisDesign-for-manufacturing approach derived from the OneWeb commercial satellite constellation
• ProductionAssembly line process at Merritt Island, Florida

Larger, more modular member of the ARROW bus family, derived from the OneWeb constellation design-for-manufacturing approach.

ARROW 150 Satellite Bus

High-volume production satellite bus for proliferated LEO constellations: 100 kg payload mass, 1 cubic metre payload volume, 250…

NEXT-C Ion Propulsion System

7 kW gridded ion propulsion system based on NASA Glenn technology, flown as a technology demonstration on NASA's…

Green Propulsion Systems (AF-M315E)

• PropellantAF-M315E green propellant (hydrazine alternative)
• Performance50 percent higher performance than a traditional hydrazine system
• CUBESAT module sizes1U to 8U

Non-hydrazine green propellant propulsion, including modular 1U to 8U CubeSat propulsion systems offering up to 750 m/s delta-v.

XR-5 Hall Thruster System

• TypeHall effect thruster subsystem
• StatusFlight proven, in service
• PlatformsAEHF constellation, Northrop Grumman GEOStar-3 and Mission Extension Vehicles, Lockheed Martin LM2100

Flight-proven Hall effect thruster subsystem used on AEHF, Northrop Grumman GEOStar-3 and Mission Extension Vehicles, and Lockheed Martin…

AEPS Advanced Electric Propulsion System

12 kW Hall thruster developed with NASA Glenn and JPL; three units will provide primary propulsion for the…