Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1982-06-28
1984-11-13
Schafer, Richard E.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
23926519, F42B 1518
Patent
active
044821077
ABSTRACT:
A control device using gas jets makes it possible to modify the flight direction of a guided missile. This device comprises an energy source supplying a gas flow to a set of fixed nozzles arranged in an annular member within which are coaxially placed movable sleeves, respectively provided with gas passage openings or ports. Means are provided for positioning these openings so as face the inlets of the nozzles, in order to divert the gas flow towards one of the nozzles.
REFERENCES:
patent: 3110228 (1963-12-01), Shramo et al.
patent: 3190584 (1965-06-01), Gire et al.
patent: 3273825 (1966-09-01), Kerner
patent: 3302890 (1967-02-01), Silver
patent: 3304721 (1967-02-01), Oppel
patent: 4265405 (1981-05-01), Takagi
patent: 4384690 (1983-05-01), Brodersen
"Thomson-Brandt"
Ryan Maureen T.
Schafer Richard E.
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