Integrated Thruster Unit
Glavkosmos
ITU-5000M includes a high-precision Thruster Orientation Mechanism (TOM) and a propulsion system based on the Modified Stationary Plasma Thruster with a discharge power of up to 5 kW. Each propulsion system consists of a thruster and a XFC Unit, pneumatic connections between which are realized by me
Technical specifications
- Nominal range of station keeping – pitching motion
- [-34⁰; +14⁰]
- Nominal range of station keeping – yaw
- [-14⁰; +14⁰]
- Nominal rotation speed
- 0.2 ⁰/s
- Resolution capability
- 0.00205 ⁰
- Qualification life of motors-gear boxes
- 10000 cycles in a full angular range; 90000 cycles in an angular range of ± 1°; 26000 cycles in an angular range of ± 5°
- Power consumption
- ≤ 50 W
- Overall dimensions
- 776х760х416 mm
- Mass
- ≤ 31 kg
About
ITU-5000M includes a high-precision Thruster Orientation Mechanism (TOM) and a propulsion system based on the Modified Stationary Plasma Thruster with a discharge power of up to 5 kW. Each propulsion system consists of a thruster and a XFC Unit, pneumatic connections between which are realized by means of stainless steel pipelines. Propellant – xenon. 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.
