Space Hardware Marketplace

Power supply system (with battery unit)

A two-module CubeSat EPS (SXC-PSS-03) consisting of a power system controller (SXC-PSU-03) and battery module (SXC-BAT-03) for solar…

Honghu 50kg-Class Satellite Platform

50kg-class space science experiment satellite platform carrying integrated electronic and electric-propulsion payloads for in-orbit thruster verification.

BEVO-2

3U CubeSat built by UT Austin's Texas Spacecraft Laboratory for GPS-based rendezvous and proximity-operations experiments as part of…

MX-9 Frontier Class Explorer

A nine-engine heavy lunar lander designed for larger payload delivery and lunar sample-return missions.

Faraday Dragon Rideshare

Find out more about our Asia-Pacific regional satellite rideshare mission.

HiK Plates / Heat Pipe Assemblies

Custom heat spreaders with embedded copper-water heat pipes offering effective thermal conductivities of 10,000–100,000 W/m·K, designed to collect…

LEXI-P GEO Multi-Mission Servicer

• Mission statusUnder development (launch-ready target: 2027)
• Target orbitGeostationary Orbit (GEO)
• DeveloperAstroscale U.S.

Astroscale's multi-mission GEO servicer providing inspection, life extension, payload upgrading, relocation, and responsible EOL disposal for most GEO…

Vireo Ka 288

Vireo Ka 288 is CesiumAstro's TRL 8, multi-beam active phased array Ka-band communications payload for proliferated LEO satellite…

OS2020-6604-06

A 6dB directional coupler with SMA female connectors covering 1-2GHz at up to 50W average power.

HyPeRsonic FLight Test (HPRFLT or Hyper Flight) service

• Speedabove Mach 5

Gilmour Space is launching a new suborbital flight test service in Australia aimed at commercial and defence customers…

PIE-SAR

• CharacteristicsAutomatic and high-accuracy SAR block adjustment
• Insar processingWhole-process InSAR processing
• Decomposition50% hierarchical decomposition

PIE-SAR is a software solution for processing and analyzing radar image data from mainstream spaceborne Synthetic Aperture Radar…

BUC/SSPA Amplifiers (C/X/Ku/Ka Band)

High power outdoor solid-state amplifiers across C, X, Ku, and Ka bands — 400W Ka-Band SSPA at 27.5-30GHz…

Transporter-Erector

• PurposeThe Transporter-Erector is intended for ILV (integrated with automated satellites, unmanned and manned spacecraft) transportation from technical complex to launch complex (and back if necessary) and its erection on the launch pad.
• Year of releaseDevelopment start 2014
• Design life15 years

The Transporter-Erector is a ground support equipment designed to transport integrated launch vehicles (ILV) from a technical complex…

Solar Panels for Small Satellites

Custom deployable solar array panels for small satellites above 12U, up to 100 kg class, with triple-junction cells…

HyperSat High-Throughput Data Downlink Architecture

• PlatformIntegrated with HyperSat LEO hyperspectral satellites
• PurposeHigh-volume hyperspectral data downlink
• Data product supported500-band Metadata Hypercubes

High-throughput optical and RF satellite communications system enabling rapid downlink of large-volume 500-band hyperspectral Metadata Hypercubes from LEO…

NSS3 Sun Sensor

Miniature, fully autonomous digital sun sensor with <0.02° precision and CubeSat Space Protocol over I2C.

On-board computer

A radiation-tolerant, dual-redundant onboard computer (SX-SBOX-OBC-01) built on a SPARC v8 Leon4FT processor with CAN, SpaceWire and optional…

ZSF200 Receptacle Connector

The ZSF200 is a receptacle connector featuring a shell size of 21 and insert arrangements including 11, 16,…