Type 1 Solar Array Drive Assembly
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Key Features:
- Design is based on Moog Type1 rotary actuator
- Integrated slip ring assembly mounted on the output of the actuator
- Integrated potentiometer position feedback
- Low weight
- Zero backlash
- Optimized for low power consumption
Specifications
Parameter | Data |
Output Step Size |
0.0375 Degrees |
Output Torque | 8.4 Nm |
Unpowered Holding Torque | 4.9 Nm |
Power | 8.6 W |
Operating Temperature Range | -30˚ C to +65˚ C |
Mass | 1.16 Kg |
Slip Ring Complement | 30 @ 2 amp derated capacity / 45 volts |
Position Sensor | Potentiometer ±0.36 degree |
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Space
Moog has designed and manufactured components and systems for satellites and launch vehicles for more than 60 years.
Spacecraft Technologies
Moog is a proven leader in components, subsystems, and systems for spacecraft of all sizes, from smallsats to GEO spacecraft. Moog has been successfully providing spacecraft controls, inspace propulsion, and major subsystems for science, military, and commercial operations for more than 60 years.