Current advances in flight propulsion technology introduce element of excessive heat encountered both in atmospheric entry, and in high speed flight within atmosphere, which threatens operation of existing flight stabilization systems which utilize dynamic response characteristics of electrohydraulic servomechanisms; possible solution to problem is provided by pneumatic control system which is able to retain stability over entire anticipated thermal range.
Space age ushers in pneumatic controls
Battelle Tech Rev
Battelle Technical Review ; 9 , n 8
1960
7 pages
Article (Journal)
English
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