Attitude Control Thruster Unit Based on Modified Thermocatalytic Low Thrusters
Glavkosmos
Propellant - hydrazine. The unit consists of two modified thermocatalytic low thrusters: 1 – main, and 1 – redundant. Thermal mode of the unit is ensured by 4 heaters (2 main and 2 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 4 temperature sensors. Manufacturin
Technical specifications
- Heater unit power consumption
- 14.6 W
- Overall dimensions
- 208х150х128 mm
- Mass
- 1.55 kg
About
Propellant – hydrazine. The unit consists of two modified thermocatalytic low thrusters: 1 – main, and 1 – redundant. Thermal mode of the unit is ensured by 4 heaters (2 main and 2 redundant), a radiator, and a set of MLI. Unit temperature is monitored by means of 4 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.
