Electrical actuator (ELA) power efficiency and requirements are examined for space system application. Requirements for Space Shuttle effector systems are presented, along with preliminary ELA trades and selection to form a preliminary ELA system baseline. Power and energy requirements for this baseline ELA system are applicable to the Space Shuttle and similar space vehicles.
Strategic avionics technology definition studies. Subtask 3-1A: Electrical Actuation (ELA) systems
1993-09-30
Report
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English