Attitude Control Propulsion Unit
- Purpose: Creating steering effort in the attitude modes and in the spacecraft survivability modes.
- Year of release: 2003
- Guaranteed service life (years): 19
- Estimated production / delivery time (months): 7
Parameter | Value |
---|---|
Operating propellant | Xenon (State Standard GOST 10219-77) |
Nominal nozzle thrust, N (gf) | 7.85×10-2 (8) |
Active lifetime, years | 15.5 |
Mass, kg, not exceeding | 0.33 |
Pneumatic automation equipment.
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