Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1983-11-28
1992-08-18
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
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
The Secretary of State for Defence in Her Britannic Majesty's Go
Tudor Harold J.
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