Space Hardware Marketplace

DMAG Digital Magnetometer

• Dynamic Field Range±65,000 nT
• Noise≤20 nT (1σ)
• Offset≤500 nT

3-axis digital magnetometer with RS-485/422 interface and ±65,000 nT range for LEO attitude reference, ITAR/EAR-free and customizable to…

Redwire FALCCON High Gain Broadband Space Antenna

Frequency Agile L-Band Core Common Node antenna delivering high-gain, broadband tactical comms, telemetry, and GNSS performance.

Redwire SpectraCAM High Resolution Flight Camera

GigE Vision LEO flight camera for docking, navigation, inspection, and situational awareness, with 5MP CMOS sensor.

Redwire Star Field Simulator

Hardware-in-the-loop star field simulator providing as-you-fly ground test operation of Redwire star trackers.

Redwire ROSA – Roll Out Solar Array

Scalable, high-power roll-out solar array using strain-energy composite booms and a rolled photovoltaic blanket, flown on ISS and…

Rigid Panel Solar Array

• Array TypeRigid panel, deployable
• Cell TechnologyHigh-efficiency triple-junction
• Orbit ApplicabilityLEO, MEO, GEO

Heritage-proven deployable rigid panel solar arrays using high-efficiency triple-junction cells for LEO, MEO, and GEO spacecraft across commercial,…

Redwire CubeStack Payload Adapter

• ConfigurationESPA-class ring adapter
• CapacityUp to 8 3U CubeSat dispensers
• Product familyRedwire Payload Adapters (with XPOD, LoFF, CubeCone)

ESPA-class ring adapter from Redwire's payload-adapter line that can hold up to eight 3U CubeSat dispensers.

Redwire CubeCone Payload Adapter

• ConfigurationTransitional ring adapter
• FunctionCan also accommodate secondary payloads
• Product familyRedwire Payload Adapters (with XPOD, LoFF, CubeStack)

Transitional conical ring adapter from Redwire's payload-adapter line that can also accommodate secondary payloads.

LoFF Low-Shock Separation System

• TypeLow-shock frangible separation system
• Shock OutputSignificantly reduced vs. traditional pyrotechnic systems
• RedundancyFully redundant initiation

Low-shock frangible separation system delivering significantly reduced pyrotechnic shock versus traditional bolt-cutters, with fully redundant initiation for launch…

Coarse Sun Sensor — Cosine Type

• Field of ViewApproximate cosine, conical symmetry
• Number of Detectors1
• Mass10 g

Miniature single-detector radiation-hardened coarse sun sensor (10 g) with approximate cosine field of view for solar array pointing…

Redwire XPOD CubeSat Deployer

• ConfigurationCustom adapter hosting 3 XPOD CubeSat dispensers
• Product familyRedwire Payload Adapters (with LoFF, CubeCone, CubeStack)
• Mission heritageORS-3, Spaceflight SSO-A, SpaceX Rideshare, Spaceflight GTO-1, SpaceIL Lunar Lander

Custom Redwire payload adapter configuration designed to host three XPOD CubeSat dispensers on a single rideshare interface.

Redwire SpectraTRAC Star Tracker

Compact, autonomous Lost-in-Space star tracker for CubeSat, NanoSat, and Spaceflight missions.

Coarse Sun Sensor — Pyramid Type

• Field of View2π steradian+
• Accuracy at Null±1°
• Accuracy (Linear Range)±5°

Radiation-hardened 4-detector pyramid coarse sun sensor with 2π+ steradian FOV and ±1° accuracy at null, requiring no external…

IRES Infrared Earth Sensor

• Operating Band14-16.25 um (thermal IR)
• Earth Acquisition Range15,300-53,000 km
• Operational AltitudeUp to 140,000 km

Two-axis infrared Earth horizon sensor for GEO/MEO 3-axis spacecraft: 14-16.25 um band, <0.05 deg accuracy, 10Hz, <2.5kg, <4W,…

Mini-PHM Passive Hydrogen Maser

• Output Frequency10.00285741 MHz (fH/142)
• Output Level+7 dBm
• Frequency Drift/Day<=1e-14 (after 1 week); <1e-15 (after 30 days)

Miniaturized space passive hydrogen maser atomic clock: 12kg, <=54W, ADEV 6.5e-13 @ 1s, <1e-15/deg C thermal sensitivity, next-gen…

PHM Passive Hydrogen Maser

• Output Frequency10.00285741 MHz (fH/142)
• Output Level+7 dBm
• Frequency Drift/Day<=1e-14 (after 1 week); <1e-15 (after 30 days)

Space passive hydrogen maser — master clock of Galileo navigation system: 18.2kg, <=70W, ADEV 1.8e-12 @ 1s, 40+…

A-STR Autonomous Star Tracker

• DetectorMPP CCD (radiation-hardened)
• FOV16.4 x 16.4 deg
• Dynamic Range1.5-5.5 Mi

Single-assembly autonomous star tracker with radiation-hardened MPP CCD: 16.4x16.4 deg FOV, 8.25 arcsec bias accuracy, 10Hz, 3.55kg, 18-year…

AA-STR Autonomous Star Tracker

• DetectorHAS APS (CMOS Active Pixel Sensor)
• FOV20 x 20 deg
• Dynamic Range1.5-5.5 Mi

Next-gen CMOS APS autonomous star tracker: 20x20 deg FOV, 2.6kg, 5.6W, 8.25 arcsec accuracy, 10Hz, first TRL-9 CMOS…