The thrusters are part of liquid jet propulsion systems intended for creation of steering forces to change spatial position of
spacecrafts.
Cyclone-3 LV thruster of 100 N thrust |
Cyclone-3 LV thruster of 30 N thrust |
Ocean-O SC thruster of 30 N thrust |
- Small mass and overall dimensions;
- Increased leak-proofness;
- Quick response;
- Long service life;
- High reliability;
- Possibility to operate continuously or in pulse mode;
- Possibility to operate on saturated and non-saturated propellants.
|
| Parameter |
Cyclone-3 LV thruster | Cyclone-3 LV thruster | Ocean-O SC thruster |
| Nominal thtrust, N | 100 | 30 |
| Specificimpulse in continuous mode of operation at nominal inlet propellant pressure, m/s |
2600 |
| Chamber pressure, MPa | 0.7 |
Propellants: - oxidizer - fuel | NTO UDMH |
| Nominal inlet propellant pressure, MPa | 1.35 |
| Nominal pressure mixture | 1.6 | 1.3 | 1.6 |
| Ensured restartability | 1300 | 4900 |
| Total burn time, s | 200 | 3600 |
| Single run duration, s | from 0.21 to 165 | from 0.21 to 600 |
| Feeding voltage,V | 28 |
| Range of working temperatures, °Ñ | from -5 to +35 |
| Mass, kg | 1.45 | 1.3 |
Experience of thrusters service in composition of Cyclone-3 LV and Ocean-O SCÎ has shown their high reliability
and effectiveness. Status of development - serial production. |