Type 2 Solar Array Drive Assembly
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Key Features:
- Design is based on Moog Type2 rotary actuator
- Integrated slip ring assembly for power and data transfer is mounted on the rear of the actuator
- Integrated potentiometer position feedback
- Low weight
- Zero backlash
- Optimized for low power consumption
Specifications
Characteristic | Data |
Output Step Size (degrees) |
0.02 |
Output Torque (N-m) | 11 |
Operating Temperature Range | -50C to 80C |
Mass (Kg) | < 3.50 including harness |
Holding Torque Powered (N) | 9 |
Holding Torque Unpowered (N) | 4.5 |
Inertia Capability (Kg.m2) | 28 |
Slip-Ring Power | 34 rings @ 3.2 A |
Slip-Ring Signal | 15 rings @ 1.0 A |
Voltage | 60 |
Position Sensor | Potentiometer ± 0.36 deg. |
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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.