TU1 Thruster Unit Based on Modified Thermocatalytic Low Thruster
Glavkosmos
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. Manufacturing lead time is given without t
Technical specifications
- Heater unit power consumption
- 7.3 W
- Overall dimensions
- 171х58х109 mm
- Mass
- 0.59 kg
About
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. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6 months).
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
