Integrated Thruster Unit
- Purpose: ITU-5000M is intended for creating the required thrust forces when forming the spacecraft operating orbit followed by station keeping within the required limits during spacecraft operation in space conditions.
- Year of release: 2008
- Guaranteed service life (years): 15
- Estimated production / delivery time (months): 14
- Flight qualification of the product: No
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| 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 |
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.
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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