Space Hardware Marketplace

PULSAR-SANT

The PULSAR-SANT is a high-performance, polarized S-band antenna designed for nanosatellites, offering a small size, low profile, and…

FHA-Mini Compact Hollow Shaft Servo Actuator

The FHA-C Mini Series is a family of extremely compact Actuators that deliver high torque with exceptional accuracy…

Satellite platform OrbiCraft-Pro 3U modification “Experimental”

An assembled and manufacturer-verified 3U CubeSat platform (article SXC3) with silicon (Si) solar panels and basic B-DOT ADCS,…

Heat Pipes (HP)

• TechnologyLatent heat of vaporization, wick return
• ApplicationsData centers, embedded electronics, batteries, power electronics

Traditional heat pipe technology providing low thermal resistance passive cooling — scalable to application size, exploits latent heat…

MASTER II Next Generation Satellite OBC

• ArchitectureModular, separated control and computing layers
• RedundancyDual-section (A/B), active/standby or dual-active modes
• FailoverHardware-driven, deterministic, no software boot required

Next-generation modular OBC with dual-section hardware redundancy, PolarFire SoC, FPGA guardian supervision and on-demand edge AI.

NANOsky CMM SDK

• ComponentsApplication Library module (Qt/C++, Windows/Linux) + FW module (C-based, RTOS)
• Compatible equipmentNANOobc-2, NANOhpm-obc, NANOlink-2, NANOcomm-2, NANOif, NANOeps, NANOamppt, picoRTU system
• Fw module functionsBootloader, FDIR, CAN-TS/LVDS-TS stacks, housekeeping TM, memory & OBT management, software scrubber

Software development kit for control, monitoring and management (CMM) of NANOsky platform subsystems.

Test Bench for Mutual Movement of Spacecraft

An aerodynamic (air-bearing) test table that lets scale mock-ups of spacecraft move freely in the horizontal plane with…

Scotty LEO User Terminal

• Network accessEnables access to Skyloom's network via GEO
• Data rateSupports LEO-GEO links up to 20 Gbps
• Field of regardHemispherical Field Of Regard

LEO user optical terminal enabling multi-Gbps LEO-to-GEO data relay via Skyloom's optical network, up to 20 Gbps.

Compute as a Service

• Compute architectureLinux / ARM
• Deployment modelContainerized customer software payloads

On-orbit edge computing letting customers run containerized software payloads directly on Xplore satellites.

Spacety Cubesat / Smallsat Platforms

• Platform sizes offered6U, 12U cubesat/smallsat buses
• Flight heritage20+ satellite missions flown
• Typical mission typesEarth observation, satellite communication, navigation, science, technology demonstration

Low-cost, high-performance cubesat and smallsat bus product line, flight-proven over 20+ missions.

Amaya Space Satellite Services

• ServicesSatellite engineering and mission support
• CountrySouth Africa

South African space technology company providing satellite engineering and mission support services for the African space sector.

Stream Ground Station

• FrequencyUp to 40 GHz broadband/multiband LEO communications
• InterfaceTransportable LEO tracking ground station

Stream is SPACE-SI's next-generation LEO tracking ground control station in Ljubljana, Slovenia, for broadband and multiband satellite communications.

MWSE Space Microwave Payloads (GASPER / FMPL-2 / GBSAR)

• Space payload: gasperGalileo-enabled in-orbit receiver for IOD/IOV missions
• Space payload: fmpl-2L-band radiometer + GNSS-Reflectometer SDR; flown on 3Cat-5/A nanosatellite
• Space payload: fsscat RF front-endL-band radiometer and GNSS-R reflectometer channels for FSSCat mission

Spanish company developing L-band radiometers, GNSS reflectometers, software-defined radio payloads and ground-based synthetic aperture radars for small satellite…

Aurora Light Spaceplane

• Length~28 meters
• StagesTwo-stage (reusable turbofan+aerospike main stage; rocket-powered upper stage)
• Orbital payload capacity1,000 kg to low Earth orbit

Aurora is POLARIS Raumflugzeuge's flagship two-stage, fully reusable spaceplane, designed for aircraft-like runway operations to deliver small/medium satellites…

200 N HPGP RCS Thruster

Reaction control system configuration of the 200 N HPGP monopropellant thruster for high-thrust attitude and orbit control.

Redwire Coarse Sun Sensor – Pyramid

2-axis, 4-detector pyramid-configuration coarse sun sensor for solar array pointing and sun acquisition.

Thermo-Modulating Heat Pipes (TMHPs)

• Working fluid / envelopeAluminum-ammonia
• Ncg reservoirIntegrated (no separate reservoir)
• Demonstrated load (VCHP Mode)~36 W

A dual-mode spacecraft thermal device combining VCHP and thermal diode functions in a single gas-charged aluminum-ammonia design, eliminating…

VRW-B-02 Reaction Wheel

Compact low-momentum reaction wheel for small satellites, 0.2 Nms angular momentum.