Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XFC Unit)
- Purpose: Spacecraft (S/C) station keeping
- Year of release: 2001
- Guaranteed service life (years): 4500 hours 3000 cycles
- Estimated production / delivery time (months): 12
- Flight qualification of the product: Yes
- Brief history of flight qualification: As part of: S/C of Cosmos series; S/C of Luch series (launched on 16.12.94, 11.10.95); Kupon S/C (launched on 16.12.94); S/C of Yamal series (launched on 06.09.99, 24.12.03); KazSat-1 (launched on 18.06.06); KazSat-2 (launched on 16.07.11); Express-MD1 (launched on 11.02.09): Express-MD2 (launched on 06.08.12); EgiptSat-F (launched 22.02.19))
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Discharge power | 669 W |
| Discharge voltage | 300 V |
| Discharge current | 2.23 A |
| Thrust | 39 мН |
| Specific impulse | 1470 s |
| Efficiency | 43% |
| Specific power | 238 W/kg |
| Power-to-thrust ratio | 17.2 W/mN |
| Total impulse | > 0.5 MN∙s |
| Mass | 2.8 kg |
Consists of two units: M-70 Stationary Plasma Thruster 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).
Legal information
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Information on this site may be changed or supplemented.
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Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XFC Unit)