Space Hardware Marketplace

Geoscan 16U CubeSat Platform (InnoSat16)

The Geoscan 16U is a microsatellite platform in the CubeSat 16U form factor developed for Earth remote sensing…

CU2

• DC disturbance field attenuation-46dB ±1 dB
• Zero field DC drift over 6 hours<100nT
• Maximum field per axis<±500μT

The CU2 Closed-Loop Module provides active compensation for external DC and AC magnetic field variations, compatible with 3-axis…

Helios and Trailblazer Launch Vehicles

Helios and Trailblazer are responsive, dedicated launch and suborbital access solutions designed for high cadence and mass production,…

S-Band Patch Antenna

The S-Band Patch Antenna is a compact, flight-proven antenna designed for robust uplink and downlink performance in small…

CubeSat Kit Upgrade to PIC24 (PIC24FJ256GA110)

• SKU711-00718
• Price$5,455.00 per item
• Hardware/software classificationDevelopment Hardware | Development Software | Flight Hardware | Flight Qualified | Space Proven

A software and hardware upgrade package adding Microchip PIC24FJ256GA110 support to an existing CubeSat Kit purchase, for customers…

MM200

The MM200 is a magnetorquer designed for small satellites, providing precise attitude control and reaction wheel desaturation.

TriSept Security Enhanced Layer

TSEL is a Linux® based operating system for embedded devices, with a focus on providing a general purpose…

Space Instruments and EO Sensors

• Key instrumentsVIIRS (JPSS weather), NIRCam (JWST primary science), Hubble ACS, WFC3, COSTAR
• Viirs22-band radiometer on NOAA Suomi NPP and JPSS satellites
• Jwst nircamPrimary science camera, 0.6–5 μm, operating at 37 K cryogenic

Ball Aerospace's electro-optical instruments for space telescopes and Earth observation satellites — including VIIRS, JWST NIRCam, and the…

Multimode Integrated Monopropellant Electrospray (MIME) Thruster

The Multimode Integrated Monopropellant Electrospray (MIME) Thruster is a propulsion system for small satellites that can operate in…

High Pressure Electric Valve

This High Pressure Electric Valve is designed for opening and closing low-pressure gas paths, suitable for applications requiring…

Space Mechanisms (SADA, Gimbals, Rotary Actuators)

• Sada — type 3/5Single-axis solar array drive; 40+ year heritage
• Sada — small satellite sade0.8 kg; 22–34 VDC; RS-422; 88.9×101.6×48.3 mm; 50 kRad TID
• Thruster gimbal (Model T)Dual-axis EP thruster pointing; GEO orbit-raise and station-keeping

Moog's space mechanisms portfolio: Solar Array Drive Assemblies with 40+ years heritage, dual-axis thruster gimbals for EP systems,…

PAS 610S (24 in) Separation System

• Interface diameter610 mm (24 in)
• CompatibilityMoog CSA ESPA; ESPA Rideshare User's Guide environments
• Release mechanismCBOD-LT Separation System Release Mechanism

Low-shock separation system whose load capability is fully compatible with the Moog CSA ESPA and the ESPA Rideshare…

Altom14 Series — LHP Evaporator Modules for Power Electronics

• MaterialStainless Steel (SS)
• Configuration options1-slot to 3-slot (1SL, 2SL, 3SL) and multi-channel variants
• Representative sizes40×160 mm (1SL), 100×140 mm (2CPL)

High-performance stainless steel Loop Heat Pipe evaporator modules for power electronics cooling — ISO 3834-2 certified welding, manufactured…

Active Weightlessness System

• PurposeGround modal testing under conditions simulating weightlessness and testing of large transformable spacecraft systems deployment, including reflectors with a diameter up to 50 m.
• Year of release2014
• Design life3 years

The Active Weightlessness System is a ground-based test equipment designed to simulate weightlessness for modal testing of large…

KSD CubeSat Deployers

CubeSat deployer systems for launch vehicle integration, supporting 1U–6U nanosatellite deployment in LEO.

Antenna-feeder Systems of the Spacecraft

• PurposeDevelopment, manufacture and testing of spacecraft antenna-feeder systems. Carrying out radio engineering tests of spacecraft of almost any dimension in anechoic chambers.
• Flight qualification of the productYes
• Brief history of flight qualificationVast work experience.

Glavkosmos offers development, manufacturing, and testing services for spacecraft antenna-feeder systems, including radio engineering tests in anechoic chambers.

VLSI 16-bit ADC with a Sampling Frequency of 200 MHz

CMOS 90 nm 16-bit 200 MSps pipeline ADC (Н18.64-2В, 2.5 V, 26.6×26.6×2.9 mm, 3 g, 85 dB SFDR,…

Tenacious Micro Rover

TENACIOUS is a lightweight micro rover developed by ispace-EUROPE (Luxembourg subsidiary), making it the first European-designed, manufactured, and…