Earth Horizon Sensor
Pyxis SpaceThe Pyxis Space Earth Horizon Sensor provides nadir-vector measurement for CubeSat attitude control using both visible (VIS) and…
5746 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
The Pyxis Space Earth Horizon Sensor provides nadir-vector measurement for CubeSat attitude control using both visible (VIS) and…
Medium-Earth-orbit navigation satellite platform proven on 34 Galileo FOC satellites at ~23,616 km altitude.
Advanced GEO technology-demonstration satellite based on SmallGEO bus, hosting flexible in-orbit verification payloads for DLR.
The Pyxis Space Reaction Wheel is a miniaturized momentum exchange device for precise attitude control of CubeSat and…
European small geostationary satellite platform for commercial telecommunications missions up to 3,500 kg launch mass.
Flexible LEO satellite platform for Earth observation and reconnaissance missions, proven on SAR-Lupe and EnMAP.
High-capacity 11,264 Wh / 288 Ah space lithium-ion battery for large satellite platforms.
Launcher-qualified prismatic MP and cylindrical VL rechargeable lithium-ion batteries for space launch vehicles.
Compact 64 Wh / 4.5 Ah space lithium-ion battery for microsatellites and nanosatellites in LEO and small GEO…
512 Wh / 18 Ah space lithium-ion battery in 8-series 4-parallel configuration for LEO and small GEO satellites.
Space-qualified D-size 16 Wh lithium-ion cell designed for LEO and GEO satellite applications.
Family of catalytic hydrazine monopropellant thrusters for satellite attitude and velocity control, spanning 0.4 N to 86 N…
Modular, ESPA-ring-based satellite bus product line with five variants (D, HP, SLV, LT, EP) spanning LEO tug, small-launch,…
Customizable Actuator for Space Precision Rotation (CASPR) family of zero-backlash rotary actuators for antenna and payload articulation, plus…
Flight-proven pulse-tube cryocooler with no moving parts in the cold end, used on NASA climate, astronomy and missile-defense…
Large-aperture deployable mesh reflector antenna, scalable from 3 to 22 meters, with over 150 years of collective on-orbit…
Fiber-optic inertial measurement unit for space applications with flight heritage on Mars rovers and deep-space probes.
Scalable rigid honeycomb-panel solar arrays from 50 W to over 15 kW per wing for LEO, MEO, GEO,…
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