Airbreathing propulsion system for supersonic vehicles

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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Details

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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