Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1978-07-28
1980-12-23
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 319, F42B 1500
Patent
active
042405963
ABSTRACT:
An articulated radome for the front end of a missile or the like comprises a generally dome or spherical shaped articulated housing mounted for rotation about two separate transverse axes, with an infra-red window surrounded by a dielectric window so that both infra-red and radar sending and sensing units may be mounted within the dome for target scanning and the like.
REFERENCES:
patent: 2972743 (1961-02-01), Svensson et al.
patent: 3069112 (1962-12-01), Patterson
patent: 3078455 (1963-02-01), Brainin
patent: 3084340 (1963-04-01), Stout et al.
patent: 3114149 (1963-12-01), Jessen, Jr.
patent: 3995933 (1976-12-01), Crowhurst
Schmid Hans-Peter
Winderman Jay B.
Baker Freling E.
General Dynamics Corporation Pomona Division
Johnson Edward B.
Jordan Charles T.
Martin Neil F.
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