GeoMicroSat (GMS) Satellite Platform
Princeton Satellite Systems
Compact ITAR-free 3-axis-stabilized geosynchronous satellite platform for internet delivery, agricultural sensing, and secure communications with automated formation flying.
Technical specifications
- Dry Mass
- 292 kg
- Solar Power
- 4.4 kW
- Design Lifespan
- 10 years
- Attitude Control
- Four reaction wheels + star camera + MEMS IMU
- Propulsion (E-W stationkeeping)
- Hydrazine thrusters
- Propulsion (N-S stationkeeping)
- Hall thrusters
- Communications (uplink/downlink)
- C-band
- Communications (cross-links)
- Ka-band
- ITAR Status
- ITAR-free
- Formation Flying
- Automated multi-vehicle navigation and stationkeeping
About
The GeoMicroSat (GMS) is a compact geosynchronous satellite platform developed by Princeton Satellite Systems that is designed to be ITAR-free, enabling international sales and partnerships. The platform supports multi-vehicle formation flying with automated navigation and stationkeeping, making it suitable for high-capacity GEO constellations.
The GMS features a dry mass of 292 kg with 4.4 kW solar power and a 10-year design lifespan. Attitude control uses four reaction wheels combined with a star camera and MEMS IMU, while propulsion combines hydrazine thrusters for momentum dumping and East-West stationkeeping with Hall thrusters for North-South stationkeeping. Communications use C-band uplink/downlink with Ka-band cross-links for inter-satellite connectivity.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
