Model Type 1 Rotary Incremental Actuator
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Key Features:
- Compact and closely integrated design
- Low weight
- Zero backlash
- Optimized for low power consumption
- Small angle permanent magnet stepper provides relatively high holding and running torque
Specifications
Parameter | Units | Basis | Data |
Output Step Angle |
Degrees | Standard | 0.0375 |
Steps per Revolution | Steps | Standard | 9600 |
Max. Output Step Rate | Steps/sec | Maximum | 400 (15) |
Backlash | Degrees | Maximum | Zero |
Operating Temperature Range | °C | Maximum | -50 to +80 |
Torsional Stiffness | lb‐in/Rad | Minimum | 20,000 |
Bending Stiffness | lb‐in/Rad | Minimum | 75,000 |
Axial Stiffness | lb/in | Minimum | 500,000 |
Radial Stiffness | lb/in | Minimum | 500,000 |
Output Load Capability Axial | lbf | Nominal | 1,080 |
Tranverse | lbf | Nominal | 1,080 |
Moment | lb-in | Nominal | 415 |
Output Torque | lb‐in | Minimum | 70 |
Unpowered Holding Torque | lb‐in | Minimum | 20 |
Powered Holding Torque | lb‐in | Minimum | 70 |
Power | Watts | Maximum | 4.5 |
Total Assembly Weight | Lb | Maximum | 1.00 |
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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.