Missile

Details Missile Missile

1994-12-01

1996-06-25

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 700

Patent

active

055292615

ABSTRACT:
A missile comprising a missile body having a missile tip housing, a seeker head mounted into the missile tip housing and a positioner which selectably positions the seeker head in either an extended, seeking, position or a retracted, cruising, position.

REFERENCES:
patent: 3924826 (1975-12-01), Reinert
patent: 3995933 (1976-12-01), Crowhurst
patent: 4079687 (1978-03-01), Mentcher
patent: 4193567 (1980-03-01), McCarty, Jr.
patent: 4240596 (1980-12-01), Winderman et al.
patent: 4291848 (1981-09-01), Clark
patent: 4640194 (1987-02-01), Witt et al.
patent: 4733609 (1988-03-01), Goodwin et al.
patent: 4952042 (1990-08-01), Pinson
patent: 5379967 (1995-01-01), Shachar

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