Nanosatellite Platform
- Purpose: - to control the separation of spacecraft and the offline monitoring of their status in orbit. - earth remote sensing, detection of earthquake precursors and disaster prevention. - calibration and adjustment of space monitoring devices, and space debris monitoring.
- Year of release: 2020
- Guaranteed service life (years): 5
- Estimated production / delivery time (months): 18
- Flight qualification of the product: No
- Brief history of flight qualification: Production and ground testing of the prototype.
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Working orbits | Low, medium and geostationary orbits |
| Weight of nanosatellite platform | 3.5 kg |
| Weight of payload | 1.5 kg |
| Power supply system capacity (average/peak) | (8/20) W |
| Attiude control | Three axial |
| Attitude control accuracy | 10 angular minutes |
| Power supply voltage | 3,2 V (5,0 V) |
| Overrall dimensions | 100 х 100 х 300 mm |
Nanosatellite platform.
Remark
Сonfiguration options:
- simple Attitude Control System (ACS) with 3 magnetic torquers (MTs);
- enhanced ACS with 3 MTs, star tracker and 3 reaction wheels;
- maneuvering platform with micro thruster.
Radiation-resistant components.
Legal information
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