Gas jet steering device and method missile comprising such a dev

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

Patent

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Details

23926519, 23926527, 23926529, 23926531, 60230, F42B 1502

Patent

active

044639210

ABSTRACT:
A steering device comprising an annular element having N exhaust nozzles and a rotary element disposed coaxially inside said annular element; the rotary element comprising M gas passageways may be positioned in MN discrete directions so as to provide a transverse thrust force orientated in one of the steering planes.

REFERENCES:
patent: 2726510 (1955-12-01), Goddard
patent: 3245620 (1966-04-01), McEwen
patent: 3273825 (1966-09-01), Kerner
patent: 3302890 (1967-02-01), Silver
patent: 3927693 (1975-12-01), Johnston
patent: 4011720 (1977-03-01), Kirschner

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