Bipropellant Thruster 11d
- Purpose: Phobos Sample Return Spacecraft
- Flight qualification of the product: Letter "O", flight use
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| 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 |
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.
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