Space Hardware Marketplace

Flywheel Aerospace Momentum Storage Systems

• TechnologyFlywheel momentum/energy storage
• ApplicationSatellite attitude control
• CountryIndia

Indian company developing flywheel-based momentum and energy storage systems for satellite attitude control applications.

K-Band Solid State Power Amplifier SSPA11201721SS

The SSPA11201721SS is a K-band GaN solid state power amplifier module delivering over 10 W saturated output power…

16U satellite structure

The NanoStruct 16U provides ample room for payloads, power, and advanced systems, enabling the development of larger and…

Twist Pin Contacts

• No. 1 outer diameter d0.72 mm
• No. 1 inner diameter d0.42 mm
• No. 1 length l01.3 mm

Military-grade twist pin contacts for circular connectors in three standard dimensions, approx. 10-15 day lead time.

HECTOR — SMA Rotary Actuator for Structural Deployment

• TechnologyShape memory alloy (SMA) rotary actuator
• TRL7
• Angular range90-180 degrees

Large-angle (90-180 deg) SMA rotary actuator for deploying booms, panels, and articulated structures on satellites and rovers —…

Launch Complex 1 (LC1) — Small Orbital Rocket Launch Site

• LocationTaiki-cho, Hiroo-gun, Hokkaido, Japan
• Latitude42.30°N
• Longitude143.26°E

Under-development orbital launch site at Hokkaido Spaceport with two launch pads (LP11, LP12), assembly buildings, and full propellant…

RGUC-U Low Power (IFL or MS)

Block Up-Converter (BUC) — RGUC-U Low Power (IFL or MS), frequency S: 14.00-14.50 GHZ E: 13.75-14.50 GHZ, output…

PicoSatellite Launcher PSL6U / PSL6U XL

The ASTROFEIN PSL6U and PSL6U XL are CubeSat deployers designed for 1U, 2U, 3U, or 6U CubeSats, featuring…

IARE Aerospace Systems Laboratory

• TypeResearch Laboratory
• SpecializationAeronautical and Aerospace Systems
• InstitutionIARE Hyderabad

The IARE Aerospace Systems Laboratory at the Institute of Aeronautical Engineering conducts research in aerospace systems, avionics, and…

Kinetica-2 (PR-2) Launch Vehicle

Next-generation kerosene/LOX medium-heavy launch vehicle rated at 12 t to LEO and 8 t to 500 km SSO.

Mosaic

• TypeMission autonomy / command-and-control software platform
• Deployment modelsCloud (GovCloud compliant), local/air-gapped network, containerized
• CompatibilityFly Jackal, third-party spacecraft, or entire constellations

Ground-up mission autonomy and command-and-control software platform for space superiority, built by former Space Force operators and software…

TiNi ERM E4000 Ejector Release Mechanism

The EBAD TiNi™ Ejector Release Mechanism E4000 is a derivative of the TiNi™ Pin Pullers, employing a Shape…

Test Bench for RASCube Modules

• CompatibilityRASCube V1, V2 and LB

The CubeSat Test Bench allows for easy testing and prototyping of RASCube modules by laying them out like…

RD809M

The RD809M is a four-chamber staged combustion cryogenic rocket engine developed by Yuzhnoye SDO for upper stage main…

LDS3507 3U OpenVPX, CMOSS/SOSA-aligned, Single Board Computer

• ProcessorIntel 12-core Xeon D processor @ 1.5 GHz
• FPGAXilinx UltraScale+ ZU19
• MemoryUp to 16 GB DDR4 memory ECC

The EnsembleSeries™ LDS3507 combines a 12-core Intel® Xeon® D processor with a Xilinx® Zynq® UltraScale+™ ZU19 FPGA to…

Slotted Waveguide Array Antenna

A custom-designed, high-gain flat antenna solution for satellite payload applications requiring gains above 20 dBi in the Ku…

Software bundles

Flight-proven, highly reliable software bundles designed for comfortable integration and easy adaptation to mission-specific needs, performing all necessary…

XLink SDR Transceiver

XLink is a flexible and flight-proven Software Defined Radio (SDR) transceiver platform for small satellites, offering high reliability…