TU1 Thruster Unit Based on Modified Thermocatalytic Low Thruster
- Purpose: Spacecraft orientation and attitude control.
- Year of release: 2013
- Guaranteed service life (years): 5
- Estimated production / delivery time (months): 12
- Flight qualification of the product: Yes
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Heater unit power consumption | 7.3 W |
| Overall dimensions | 171х58х109 mm |
| Mass | 0.59 kg |
Propellant - hydrazine. The unit consists of one modified thermocatalytic low thruster. Thermal mode of the unit is ensured by 2 heaters (1 main and 1 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 3 temperature sensors.
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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