Space Platform 50
- Purpose: Design and manufacture of small spacecraft for technological scientific and educational purposes in low circular orbits.
- Year of release: 2012
- Guaranteed service life (years): At least 1 year (with bringing SAS up to 5 years).
- Estimated production / delivery time (months): 12
- Flight qualification of the product: Yes
- Brief history of flight qualification: The prototype of the platform is part of the ICA "MIR" (launched July 28, 2012).
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Working orbits | Low circular orbit (from 400 to 1500 km) with associated launch |
| Platform weight | Up to 30 kg |
| Payload weight | Up to 40 kg |
| Payload power supply capacity | Average (30 W); peak (90 W) to 10 min. |
| Orientation | Three-axis, active |
| Orientation accuracy, deg | ±10 |
| Nominal voltage, V | 27±0,5 |
Platform for small satellites weighing up to 70 kg. the Height of the orbit is 1500 km.
Peculiar properties:
- untight;
- nickel-metal hydride battery (its elements are part of a single onboard control system);
- passive thermal control system on heat pipes and heaters;
- the motion control system of a SPACECRAFT on electromagnetic devices;
- propulsion system on hydrazine (can also be gas). Installed on demand;
- a single onboard control system.
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