Cool Gas Thruster
- Purpose: KOSMOS and RESURS-DК spacecraft
- Flight qualification of the product: Letter "O", flight use
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Working medium | helium/nitrogen |
| Nominal Thrust | 0.733/0.819 N |
| Nominal Specific Impulse, Steady State | 1657.9/716.1 m/s |
| Nominal Inlet Pressure | 1.765 MPa |
| Inlet Operating Pressure | 1.47…1.96 MPa |
| Total Firing Time, up to | 10,000 s |
| Cycle Life, Number of Starts-up, up to | 80,000 |
| Nozzle Expansion Ratio | 64 |
| Operating Voltage | 27 V |
| Mass, not over | 0.105 kg |
Formation of multiple impulses for precise orientation of spacecraft in response to control system triggering commands. Design features: - Small size and mass.
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