Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1972-11-30
1982-05-04
Bentley, Stephen C.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
60245, 60251, 60270R, 137 151, 23926515, F42B 1516
Patent
active
043278868
ABSTRACT:
A two-stage aerial vehicle which is launched and accelerated by an integral olid booster. After booster burnout and jettison of the booster nozzle, the booster chamber becomes the combustion chamber for a liquid fueled ramjet. The vehicle is designed for use with known guided missile launching systems and employs unique ram air scoop and control surface actuator structure.
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Bell Alfred J.
Cronvich Lester
Hardgrave, Jr. Everett J.
Polk, Jr. Albert S.
Bentley Stephen C.
Branning A. L.
Sciascia R. S.
The United States of America as represented by the Secretary of
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