Bipropellant Thruster
Glavkosmos
Formation of multiple impulses for attitude control of spacecraft in response to control system triggering commands.
Technical specifications
- Propellants, Fuel/Oxidizer
- UDMH/NTO
- Nominal Thrust
- 392 N
- Nominal Specific Impulse, Steady State
- 2,989 m/s
- Nominal Inlet Pressure
- 1.47 MPa
- Inlet Operating Pressure
- 1.27…1.97 MPa
- Total Firing Time, up to
- 1,000 s
- Cycle Life, Number of Starts-up, up to
- 10,000
- Nozzle Expansion Ratio
- 100
- Operating Voltage
- 27 V
- Mass, not over
- 3 kg
About
Formation of multiple impulses for attitude control of spacecraft in response to control system triggering commands.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
