Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1979-12-17
1983-01-25
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
60204, 60270R, 244 31, 244 53A, F42B 1502
Patent
active
043699405
ABSTRACT:
A propulsion system for airbreathing vehicles having a ducted inlet for a supersonic powerplant and incorporating means in the vehicle for momentarily changing the normal flight attitude of the vehicle for obtaining high inlet pressure recovery for the propulsion powerplant and thereafter returning the vehicle to a normal flight attitude.
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Arcangeli Gerald T.
Kelly Patrick J.
McDonnell Douglas Corporation
Tudor Harold J.
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