- Purpose:
- Creation on the platform base of small spacecrafts for different scientific purposes
- Areas of possible application:
- Carrying out of fundamental scientific researches; Earth remote sensing; Testing of new technologies and software and hardware solutions; meteorological and environmental monitoring; communication providing; small spacecraft constellation of different target purpose etc.
- platform mass:
- up to 140 kg
- Orientation:
- three-axes
- average daily power supply system capacity:
- up to 250 W;
- onboard radio complex frequency range:
- S (Х)
- propulsion system:
- ablative pulsed plasma
- SC on the module base:
- MKA-FKI (PN1), Zond-PP, MKA-FKI (PN2), Relek
- P/L mass:
- up to 100 kg
- Injection into the orbit:
- Piggyback as additional P/L or batch. Variant of transportation mean – Soyuz LV with Fregat upper stage
- Operational orbits:
- Low earth orbit with different inclination. Possible usage in high elliptical orbits
