Spacecraft Mechanisms

Micro3 Rotary Incremental Actuator

Micro3 Rotary Incremental Actuator
  • Compact, closely integrated design made up of a motor and harmonic drive speed reducer
  • Motor is a small angle permanent magnet stepper with relatively high holding torque
  • Co-axial nesting of the motor and harmonic drive elements gives the unit low profile geometry
  • All electrical elements such as motors and position sensors can be redundant with little or no charge in actuator envelope
Specifications Units Basis Data
Output Step Angle Degrees Nominal 0.0009375
Steps / Revolution - Standard 384,000
Max. Output Step Rate Step/sec (Deg/sec) Maximum 640 (0.6)
Nominal Step Rate for LEO APM Applications Step/sec (Deg/sec) Standard 80 (0.075)
Torsional Stiffness Lb-in/rad (Nm/rad) Maximum 150,000 (17,000)
Output Torque at Nominal Speed Lb-in (Nm) Standard 800 (90)
Holding Torque Unpowered Lb-in (Nm) Maximum >1100 (>120)
Holding Torque Powered Lb-in (Nm) Maximum >1100 (>120)
Power Dissipation Watts Nominal 3.0
Total Assembly Weight Lb (grams) Nominal 3.40 (1542)

Our extensive product offering of Rotary Actuators are flexible and customizable to your specific needs. For more information on Rotary Actuators, or this specific model please contact our Chatsworth facility.

Micro3 Rotary Incremental Actuator Datasheet

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Spacecraft Mechanisms Product Catalog

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For Additional Information Regarding our Spacecraft Products:

Philip Tokeshi

Spacecraft Mechanisms Sales Manager

+1-818-734-6770