Seeker head assembly in a guided missile

Details Seeker head assembly in a guided missile Seeker head assembly in a guided missile

1992-04-10

1994-12-13

Tudor, Harold J.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

62239, 102293, 244117A, 244158A, 250238, B64G 158, F41G 700

Patent

active

053723333

ABSTRACT:
In a seeker head assembly in a guided missile, particularly a high-speed guided missile, the seeker head (22) is covered by a dome (28) which is rotatably mounted in the structure and is rotated. The dome (28) is circumferentially surrounded by the structure (10) of the guided missile except for a window section (14). A coolant is supplied to an interspace (46) formed between dome (28) and structure (10) of the guided missile.

REFERENCES:
patent: 2823612 (1958-02-01), Cox et al.
patent: 3080816 (1963-03-01), Levine
patent: 3762666 (1973-10-01), Thompson
patent: 3974985 (1976-08-01), Campbell et al.
patent: 4057104 (1977-11-01), Altoz
patent: 4235398 (1980-11-01), Johnson
patent: 4702439 (1987-10-01), Kelley et al.
patent: 4717822 (1988-01-01), Byren

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