TU3 Truster Unit Based on Modified Thermocatalytic Low Thrusters
- 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 | 232х179,5х79,5 mm |
| Mass | 1.3 kg |
Propellant - hydrazine. The unit consists of three modified thermocatalytic low thrusters. Thermal mode of the unit is ensured by 3 heaters (2 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).
Legal information
Please note that this site is for informational purposes only and under no circumstances is not a public offer determined by the provisions of the Part 2 Article 437 of the Civil code of the Russian Federation.
Information on this site may be changed or supplemented.