Propulsion System [PS] for Nanosatellite Platform
- Purpose: Orbital maneuvering of cubesat-class spacecraft.
- Year of release: 2016
- Guaranteed service life (years): 3
- Estimated production / delivery time (months): 12
- Flight qualification of the product: No
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Stock of characteristic velocity for nanosatellite with weight up to 5 kg | up to 25-30 m/s |
| The total mass of PS | 1,3 kg |
| Minimum energy consumption | 3 - 5 W |
| Maximum power consumption | 12 W |
| Working body weight | up to 0,2 kg |
| Supply voltage | 5 - 12 V |
| Preparation time for start of the PS (preheating) | 60 s |
| The maximum time of a single inclusion to generate thrust | up to 1200 s |
| Electrothermal engine thrust | 0,003 - 0,01 N |
| Overall dimensions | 91 х 96 х 130 mm |
- Electrothermal propulsion unit for nanosatellite platform.
Legal information
Please note that this site is for informational purposes only and under no circumstances is not a public offer determined by the provisions of the Part 2 Article 437 of the Civil code of the Russian Federation.
Information on this site may be changed or supplemented.