GIMBAL RETRACTION MECHANISM

FOR MANNED AND UNMANNED AIRCRAFT

Optimized for High Accelerations

Technical specifications

Specifications

  • <10 - 14 V
  • 7W during actuation, 0.6W when deployed/retracted
  • < 450 grams
  • < 1 second
  • CAN / PWM / discrete input
  • Over-current protection ; Up/down position status indication

GIMBAL RETRACTION MECHANISM

For Manned and Unmanned Aircraft

Optimized for High Accelerations

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