Satellite Platform CubeSat 3U
- Purpose: Designed for scientific and educational missions.
- Year of release: 2018
- Guaranteed service life (years): 1
- Estimated production / delivery time (months): 5
- Flight qualification of the product: No
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Target orbit | LEO up to 650 km |
| Active lifetime, months, not less than | 6 |
| Dimensions, mm | 108х108х340,5 |
| Mass (assembled, w/o payload) kg, not more than | 1.5 |
| Available space for payload, mm | 80*70*220 |
| Accumulator capacity, W*h, not less than | 39 |
| On-board interface | CAN2.0 B |
| Available average power consumption of payload per orbit, W, not less than | 1 |
| Transmitter power, W | 1 |
| Radiochannel speed, half-duplex, bps | 9600 |
Assembled, verified and fully tested by the manufacturer satellite platform CubeSat 3U. Payload integration is possible before tests.
Contents:
- side Si solar panels with coils – 12 pcs.;
- end edge Si solar panels with coils – 2 pcs.;
- power supply system (with battery unit) – 1 pc.;
- motherboard – 1 pc.;
- computer - 1 pc.;
- UHF tranceiver – 1 pc.;
- structure CubeSat 3U – 1 pc.;
- protective covers – 6 pcs.;
- UHF antenna with service panel – 1 pc.;
- charger – 1 pc.;
- transportation case for 3U – 1 pc.
Legal information
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