Correction Unit (CU) based on Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W and XFC Unit
- Purpose: Spacecraft station keeping. Spacecraft orbit raising to GEO
- Year of release: 1995
- Guaranteed service life (years): 9000 hours 5000 cycles
- Estimated production / delivery time (months): 10
- Flight qualification of the product: Yes
- Brief history of flight qualification: As part of: S/C of Cosmos series; SS/Loral’s S/C.
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Discharge power | 1350 W |
| Discharge voltage | 300 V |
| Discharge current | 4.5 A |
| Thrust | 83 mN |
| Specific impulse | 1600 s |
| Efficiency | 45% |
| Specific power | 208 W/kg |
| Power-to-thrust ratio | 16.3 W/mN |
| Total impulse | > 2.6 MN∙s |
| Mass | 6.5 kg |
Consists of two units: Stationary Plasma Thruster with a nominal discharge power of 1350 W and Xenon Flow Controller Unit (XFC Unit). Propellant - xenon.
Remark
Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6 months).
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Correction Unit (CU) based on Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W and XFC Unit