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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
ParameterValue
Operating propellantXenon (State Standard GOST 10219-77)
Nominal nozzle thrust, N (gf)7.85×10-2 (8)
Active lifetime, years15.5
Mass, kg, not exceeding0.33

Pneumatic automation equipment.