Redwire Rigid Panel Solar Array Systems
Redwire CorporationScalable rigid honeycomb-panel solar arrays from 50 W to over 15 kW per wing for LEO, MEO, GEO,…
19 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Scalable rigid honeycomb-panel solar arrays from 50 W to over 15 kW per wing for LEO, MEO, GEO,…
Custom Redwire rideshare adapter that hosted 48 3U CubeSats on a single launch for the Spaceflight SSO-A mission.
Ground test stimulator system using infrared LEDs to optically verify sun sensor functionality, sun angles, and flight harnesses.
Small, lightweight single-detector sun sensor with cosine-symmetric field of view for solar-array pointing and sun acquisition.
2-axis, 4-detector pyramid-configuration coarse sun sensor for solar array pointing and sun acquisition.
SADA-compatible rigid solar array wing built for ESPA-class electric propulsion smallsat missions, using metallic tape-spring hinges.
Frequency Agile L-Band Core Common Node antenna delivering high-gain, broadband tactical comms, telemetry, and GNSS performance.
Hardware-in-the-loop star field simulator providing as-you-fly ground test operation of Redwire star trackers.
GigE Vision LEO flight camera for docking, navigation, inspection, and situational awareness, with 5MP CMOS sensor.
Scalable, high-power roll-out solar array using strain-energy composite booms and a rolled photovoltaic blanket, flown on ISS and…
Heritage-proven deployable rigid panel solar arrays using high-efficiency triple-junction cells for LEO, MEO, and GEO spacecraft across commercial,…
ESPA-class ring adapter from Redwire's payload-adapter line that can hold up to eight 3U CubeSat dispensers.
Transitional conical ring adapter from Redwire's payload-adapter line that can also accommodate secondary payloads.
Low-shock frangible separation system delivering significantly reduced pyrotechnic shock versus traditional bolt-cutters, with fully redundant initiation for launch…
Custom Redwire payload adapter configuration designed to host three XPOD CubeSat dispensers on a single rideshare interface.
Miniature single-detector radiation-hardened coarse sun sensor (10 g) with approximate cosine field of view for solar array pointing…
Radiation-hardened 4-detector pyramid coarse sun sensor with 2π+ steradian FOV and ±1° accuracy at null, requiring no external…
Compact, autonomous Lost-in-Space star tracker for CubeSat, NanoSat, and Spaceflight missions.
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