Space Hardware Marketplace

Custom Metal Optical Mirrors

• Mirror typesFlat, spherical, aspherical, freeform
• MaterialsAluminum, AlSi, gold, copper, NiP, crystals, polymers
• Standard diameterUp to 600 mm (larger on request)

Flat, spherical, aspherical, and freeform mirrors machined directly from metal for space and scientific optical systems.

Amun

• Operating temperature-40 C to +85 C
• Dimensions95.9 x 90.2 x 19.7 mm (0.2U)
• Mass185 g

PC/104 form-factor power management unit for 0.5U-2U CubeSats.

Ra

• Operating temperature-40 C to +125 C
• Efficiency> 30%
• Configurations1U / 2U / 3U / 6U / 8U plus custom design

High-efficiency, customizable solar panels for nanosatellites, offered in 1U-8U and custom configurations.

SchoolSat AMOS

• Size1U CubeSat (10x10x13.5 cm)
• Main boardArduino Nano
• Power board32 GB storage, 2x Li-ion 3200 mAh batteries, 3.3 V/5 V

Arduino-compatible 1U nanosatellite educational kit with real subsystems for STEM learning.

Lodestone

• Operating temperature-40 C to +85 C
• Dimensions22 x 20 x 6 mm
• Mass< 10 g

Compact combined magnetometer, gyroscope, and accelerometer module for nanosatellite attitude determination.

Murgas

• Operating temperature-40 C to +85 C
• Dimensions67 x 42 x 7.5 mm
• Mass25 g

UHF/VHF transceiver for dependable, long-range TT&C communication in space.

SAM Deployable Antenna

Deployable VHF/UHF antenna system for CubeSat TT&C communications with dipole and turnstile configuration options.

Zenith

• Operating temperature-40 C to +85 C
• Dimensions50 x 50 x 8.8 mm (customizable)
• Mass20 g

High-performance ceramic patch antenna for GNSS reception in nanosatellite missions.

Celeste

• Operating temperature-40 C to +85 C
• Dimensions67 x 42 x 7.5 mm
• Mass25 g

GNSS receiver providing precise positioning, navigation, and timing for CubeSat missions.

Eddie

• Operating temperature-40 C to +85 C
• Dimensions67 x 42 x 7.5 mm
• Mass25 g

Flight-proven on-board computer for command and data handling and payload processing in small satellite missions.

Deep Thought

• Operating temperature-40 C to +85 C
• Dimensions67 x 42 x 7.5 mm
• Mass25 g

Advanced flight-proven on-board computer for command and data handling and payload processing in any space application.

Semiconductor Materials (Diamond, GaN, AlxN)

• MaterialsDiamond, gallium nitride (GaN), aluminum nitride (AlxN)
• Manufacturing environmentMicrogravity, in-orbit chemical vapor deposition
• Target applicationsPower electronics, RF devices, advanced semiconductor markets

High-value semiconductor materials (diamond, gallium nitride, aluminum nitride) grown in microgravity for advanced electronics applications.

In-Space Growth Tool

• ProcessChemical vapor deposition (CVD)
• EnvironmentUltra-high vacuum, approximately 10^-11 Pa
• ApplicationMicrogravity crystal growth for semiconductor materials

Flexible chemical vapor deposition (CVD) tool for growing semiconductor crystals in microgravity aboard ForgeStar.

Pridwen

• DesignNon-ablative, shuttlecock-style deployable heat shield
• FunctionAtmospheric reentry protection for in-space-manufactured payload recovery
• Flight heritageParabolic flight deployment test (May 2025); operational on ForgeStar-1 (June 2025)

Non-ablative, shuttlecock-style deployable reentry heat shield enabling in-space-manufactured payloads to survive atmospheric reentry.

ForgeStar

• FunctionReusable in-space manufacturing and return platform
• PayloadChemical vapor deposition (CVD) semiconductor growth reactor
• Recovery methodPridwen non-ablative reentry heat shield

Reusable in-space manufacturing platform for growing high-value semiconductor materials in microgravity and returning them to Earth.

SPmg

• Temperature range4-37 C (active heaters prevent liquid freezing)
• Pressure1 bar
• RadiationShielded

Robust, simple 2U microgravity lab system for free-orbit satellites and ISS modules.

Fluid Management System (SPuMP / D-Pump)

• Flow rate10-500 microliters/minute
• SPuMP2 ml syringe pump, step-motor operated, temperature-controlled reservoir; up to 4 independently controlled
• D-PumpDiaphragm pump, temperature-controlled 1.2 ml reservoir, hydraulically driven by a SPuMP

Miniaturized precision pumping systems providing non-pulsating, positive-displacement, air-bubble-free fluid delivery for microgravity lab hardware.

SPAd-ISS

• Size3U-6U
• Liquid channels16-32 distinct liquid channels handling system
• Flow reactors2-6

Advanced miniaturized laboratory module for biology and biochemistry experiments aboard the International Space Station.