Adjustment and Braking Engine
Glavkosmos
Propulsive burn formation for center of mass velocity variation during spacecraft orbit control and braking.
Technical specifications
- Propellants, Fuel/Oxidizer
- UDMH/NTO
- Total Nominal Thrust
- 464.0 N
- One Thruster Nominal Thrust
- 116.0 N
- Nominal Specific Impulse of Thruster, Steady State
- 2,855 m/s
- Nominal Inlet Pressure
- 1.47 MPa
- Inlet Operating Pressure
- 1.37…1.57 MPa
- Total Firing Time, up to
- 2,000 s
- Cycle Life, Number of Starts-up, up to
- 5,000
- Nozzle Expansion Ratio
- 53
- Operating Voltage
- 27 V
- Mass, not over
- 8.0 kg
About
Propulsive burn formation for center of mass velocity variation during spacecraft orbit control and braking.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
