Solar Array Drive Mechanism. Type 4
- Purpose: Rotation of solar array wings at the specified rate; electrical power transmission for control and telemetry signals; shaping and generating signals of the output shaft rotation angle.
- Year of release: 2000
- Guaranteed service life (years): 15.5
- Estimated production / delivery time (months): 12
- Flight qualification of the product: Yes
- Brief history of flight qualification: Amos-5, Telcom-3, KazSat-3, Express-АТ1, Express-АТ2, Express-АМ8, Loutch-5A, Loutch-5B, Loutch-5V.
- Possibility to adapt the product to customer requirements: Yes
Parameter | Value |
---|---|
Output shaft rotation rate,deg/min | 0-16 |
Angle measurement error, not exceeding, ° | 2.5 |
Total current of power current-collecting devices, A | 90 |
Number of power supply circuits, units | 18 |
Overall dimensions, mm | 156 х 260 х 223 |
Number of telemetry circuits, units | 15 |
Operational life defined by hours, not less than | 150000 |
Mass, kg | 4.3 |
Electromechanical solar array drive mechanism.
Remark
Operating regime: continuous rotation.
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.