Type M8 Rotary Incremental Actuator
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Key Features:
- Very compact and closely integrated coaxial design
- Relatively high holding torque for its size
- High gear ratio provides fine step resolution
- Low weight
- Zero backlash
Specifications
Parameter | Units | Basis | Data |
Output Step Angle |
Degrees | Standard | 0.050, 0.075 or 0.150 |
Max. Output Step Rate | Steps/sec | Maximum | 600 |
Backlash | Degrees | Maximum | Zero |
Operating Temperature Range | °C | Maximum | -45 to +65 |
Torsional Stiffness | lb‐in/Rad (Nm/Rad) | Minimum | 3800 (430) |
Bending Stiffness | lb‐in/Rad (Nm/Rad) | Minimum | 45000 (5084) |
Axial Stiffness | lb/in (N/m) | Minimum | 250000 (43.9 x 106 ) |
Radial Stiffness | lb/in (N/m) | Minimum | 130000 (22.8 x 106 ) |
Output Load Capability Axial | lbf (N) | Nominal | 158 (700) |
Tranverse | lbf (N) | Nominal | 158 (700) |
Output Torque | lb‐in (Nm) | Minimum | 25 (2.82) |
Unpowered Holding Torque | lb‐in (Nm) | Minimum | 14 (1.58) |
Powered Holding Torque | lb‐in (Nm) | Minimum | 25 (2.82) |
Power | Watts | Maximum | 20 |
Total Assembly Weight | lb (Grams) | Maximum | 0.77 (350) |
Winding Type | Redundant if Required | Redundant if Required | 2 or 3 phase |
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Space
Moog has designed and manufactured components and systems for satellites and launch vehicles for more than 60 years.
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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.