Pallada Microsatellite Platform
Sputnix
Microsatellite bus for spacecraft of 80–200 kg, providing service systems and accommodation for a wide range of payloads independent of the target-instrument configuration. Designed for high-resolution Earth observation and other LEO missions.
Technical specifications
- Platform class
- Microsatellite bus, 80–200 kg spacecraft
- Orbit
- LEO, 500–800 km
- Design lifetime
- ≥ 3 years
- Platform mass (instruments)
- ≤ 120 kg
- Payload mass
- ≤ 80 kg
- Bus voltage
- 27 V
- Solar array power (max)
- up to 500 W
- Average orbital power
- up to 250 W
- TT&C (S-band)
- 1 / 0.5 Mbit/s, CCSDS
- Payload downlink (X-band)
- up to 1500 Mbit/s, DVB-S2
- ADCS
- 3-axis; pointing ±0.05°, attitude determination ≤ 30″, stabilization ±0.001°/s
- Interfaces
- SpaceWire, CAN 2.0B, LVDS
About
Microsatellite bus for spacecraft of 80–200 kg, providing service systems and accommodation for a wide range of payloads independent of the target-instrument configuration. Designed for high-resolution Earth observation and other LEO missions.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
