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
198 pages
Report
No indication
English