Space Hardware Marketplace

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…

Hydrazine Monopropellant Rocket Engines

Hydrazine monopropellant engine family from 0.02 lbf to 700 lbf thrust, with more than 19,000 units delivered.

AMBR 556 N Dual Mode High Performance Rocket Engine

556 N (125 lbf) Advanced Materials Bipropellant Rocket dual mode high performance engine for deep space and GEO…

R-42DM 890 N Dual Mode High Performance Rocket Engine

890 N (200 lbf) dual mode high performance rocket engine for spacecraft orbit raising and maneuvering.

R-42 890 N Bipropellant Rocket Engine

890 N (200 lbf) storable bipropellant rocket engine for orbit raising and in-space maneuvering.

R-6F 22 N Bipropellant Rocket Engine

22 N (5 lbf) storable bipropellant rocket engine for fine in-space maneuvering and attitude control.

R-1E 110 N Bipropellant Rocket Engine

110 N (25 lbf) storable bipropellant rocket engine for in-space maneuvering and attitude control.