High Power Type 5 Solar Array Drive Assembly
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Key Features:
- Design is based on MoogType5 rotary output stage
- 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
- Slip ring assembly capable to 6A derated current for power circuits
Specifications
Parameter | Units | Basis | Data |
Output Step Angle |
Degrees | 聽 聽 聽 聽 Standard聽 聽 | 聽 聽 0.0075聽 聽 聽 聽 聽 聽 |
Steps per Revolution | Steps | Standard | 48000 |
Max. Output Step Rate | Steps/sec (Deg/sec)聽 | Maximum | 300 (2.25) |
Backlash | Degrees | Maximum | zero backlash |
Operating Temperature Range | 掳颁 | Maximum | -50 to +70 |
Torsional Stiffness | lb-in/Rad | Minimum | 250,000 |
Moment Stiffness | lb-in/Rad | Minimum | 500,000 |
Axial Stiffness | lb/in | Minimum | 200,000 |
Radial Stiffness | lb/in | Minimum | 800,000 |
Output Load Capability Axia | lbf | Nominal | 370 |
Radial Stiffness | lbf | Nominal | 370 |
Moment | Lb-in | Nominal | 430 |
Output Torque | Lb-in | Minimum | 400 |
Mechanical Accuracy | Degrees | Better than | +/- 0.02 |
Unpowered Holding Torque | Lb-in | Minimum | 300 |
Powered Holding Torque | Lb-in | Minimum | 600 |
Slip-Ring Signal Circuits | 16 Rings derated at 1 A each | 16 Rings derated at 1 A each | 16 Rings derated at 1 A each |
Actuator Power Consumption | Watts | Maximum | 20 |
SADA Weight (without Harness) | Lb | Maximum | 11.00 |
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Space
Mooghas designed and manufactured components and systems for satellites and launch vehicles for more than 60 years.
Spacecraft Technologies
Moogis a proven leader in components, subsystems, and systems for spacecraft of all sizes, from smallsats to GEO spacecraft. Mooghas been successfully providing spacecraft controls, inspace propulsion, and major subsystems for science, military, and commercial operations for more than 60 years.