Bipropellant Thruster 11d
Glavkosmos
Formation of multiple impulses for attitude control of spacecraft in response to control system triggering commands. Design features: - A high temperature Niobium alloy nozzle with disilicide oxidation resistant coating.
Technical specifications
- Propellants, Fuel/Oxidizer
- UDMH/NTO
- Nominal Thrust
- 53.9 N
- Nominal Specific Impulse, Steady State
- 2,842 m/s
- Nominal Inlet Pressure
- 1.18 MPa
- Inlet Operating Pressure
- 1.03…1.32 MPa
- Total Firing Time, up to
- 5,750 s
- Cycle Life, Number of Starts-up, up to
- 100,000
- Nozzle Expansion Ratio
- 50
- Operating Voltage
- 27 V
- Mass, not over
- 1.5 kg
About
Formation of multiple impulses for attitude control of spacecraft in response to control system triggering commands. Design features: – A high temperature Niobium alloy nozzle with disilicide oxidation resistant coating.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
