Space Hardware Marketplace

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.

R-4D-11 490 N Bipropellant Rocket Engine

490 N (110 lbf) bipropellant rocket engine from the R-4D family originally developed for the Apollo programme.

R-4D-15 HiPAT 445 N High Performance Rocket Engine

445 N (100 lbf) high performance bipropellant apogee engine, available in dual mode configuration; the R-4D lineage is…

Satellite Multi-Layer Insulation (MLI)

Custom satellite MLI blankets for 1 K to 1800 K, with MMOD and ATOX protection options, produced for…

COOLCAT Cryogenic Superinsulation

• Coolcat 2 nw10 layers double-sided aluminized perforated polyester foil interleaved with 10 layers of non-woven polyester spacer; used in serial MRI, NMR and accelerator cryostats
• Coolcat 2 nfGlass fibre fleece spacer with 9 micrometre pure aluminium foil; high temperature tolerant, non-flammable, ISO 21010 tested
• Coolcat 2 lox5 layers pure aluminium foil with 5 layers glass fibre cloth spacer; liquid oxygen compatible, ISO 21010 tested, free of organic constituents

Multi-layer vacuum superinsulation line for cryogenic applications, laser-cut to shape, with polyester, aluminium-foil, LOX-compatible and tape variants.

Conductive Glass Fabric High-Temperature Vacuum Insulation

• Maximum temperatureUp to 550 degrees C
• TypeHigh temperature vacuum insulation, conductive glass fabric
• Advantages over ceramic fabricsGreater flexibility, no hazardous components, adjustable performance

Flexible high-temperature vacuum insulation for launchers up to 550 degrees C, free of hazardous components and tunable to…

Flexible Thermal Protection for Launchers

• Maximum temperatureUp to 1500 degrees C
• MaterialsCoated or laminated ceramic fabric and ceramic felt insulators
• ApplicationComponents in direct vicinity of rocket motors or nozzles

Coated or laminated ceramic fabric and ceramic felt insulation protecting components near rocket motors and nozzles at up…

Multipurpose Satellite Platform

Payload-agnostic 150-250 kg LEO platform with electric propulsion, ~1 kW power, low-drag profile and stackable multi-launch configuration.

Spacecraft Lifting Devices

• ActuationElectrical or manual
• Hoisting axisFixed, or convertible between horizontal and vertical configuration
• OptionsRemote control for lifting, centre-of-gravity adjustment

Electrical or manual lifting devices for instruments and spacecraft of all sizes, with fixed or convertible hoisting axis…

Satellite Transport and Shipping Containers

• Container typesHat-off, tilt-lid, door-type roll-in, large An124-compatible, constellation-type
• Thermal controlFull active and passive thermal control
• Environmental controlAir filtering and drying or N2 purging

Pressurized and non-pressurized spacecraft containers with thermal control, dynamic damping and air filtering, certified for air transportation.

SCO-M Spacecraft Container Mega

• Product lineBeyond Gravity spacecraft containers (SCO)
• Thermal controlFull active and passive thermal control
• Environmental controlAir filtering and drying or N2 purging

Large-format spacecraft transport container from Beyond Gravity's spacecraft container line, for the biggest geosatellites and deep space spacecraft.

Composite Payload Fairings

• Diameter range0.7 m to 5.4 m
• ConstructionAluminium honeycomb core with carbon fibre reinforced composite cover layers
• ManufacturingAutomated industrial process, no autoclave required

Composite payload fairings from 0.7 m to 5.4 m diameter, used on Ariane, Vega, Atlas, Vulcan and H3,…

GSE Clampband

• Clampband pas 937 sManufactured per Ariane 5 User's Manual (Issue 5 Rev 2), Soyuz User's Manual (Issue 2 Rev 1) and Vega User's Manual (Issue 4 Rev 0)
• Clampband pas 1194 vsManufactured per Ariane 5 User's Manual (Issue 5 Rev 2) and Soyuz User's Manual (Issue 2 Rev 1)
• Clampband pas 1666 mvsManufactured per Ariane 5 User's Manual (Issue 5 Rev 2) and Soyuz User's Manual (Issue 2 Rev 1)

Ground support equipment clampband connecting spacecraft interface rings to test adapters during AIT, in PAS 937 S, 1194…