Guided missiles

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

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Details

244 31, 244 324, 244 45A, 244 47, 244206, F41G 700, F42B 1501

Patent

active

051392151

ABSTRACT:
A fuselage, particularly of a guided missile, having a rotatable nose body carrying a pair of similar strakes symmetricaly disposed about the body and for anchoring incidence generated vortices thereon.

REFERENCES:
patent: 3195462 (1965-07-01), Petre
patent: 3196794 (1965-07-01), Meade
patent: 3262655 (1966-07-01), Gillespie, Jr.
patent: 4198016 (1980-04-01), Wilson
patent: 4351503 (1982-09-01), Drori
patent: 4373688 (1983-02-01), Topleffe

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