Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1975-01-06
1992-01-21
Carone, Michael J.
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
244 63, F42B 1066
Patent
active
050822020
ABSTRACT:
A jet vane thrust vector control unit is provided to pitch a missile over to a generally horizontal path after the missile has been vertically launched. A collar affixed to the base of the missile by explosive bolts is utilized to mount the unit so that the unit can be jettisoned after it has done its job.
REFERENCES:
patent: 2644296 (1953-04-01), Sanz et al.
patent: 3139033 (1964-06-01), Geissler et al.
patent: 3141409 (1964-07-01), Travis et al.
patent: 3430900 (1969-03-01), Turner et al.
patent: 3850387 (1974-11-01), Bjornson et al.
patent: 3867893 (1975-02-01), Saholt
Carone Michael J.
Forrest, Jr. John L.
Gilbert Harvey A.
Sliwka Melvin J.
The United States of America as represented by the Secretary of
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