Guided missile and fuze system therefor

Details Guided missile and fuze system therefor Guided missile and fuze system therefor

1976-03-25

1983-12-13

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 722

Patent

active

044201290

ABSTRACT:
In a guided missile, in which an altitude-sensing control causes the miss to descend to a predetermined constant low altitude at a specified time before reaching a target ship, a timing mechanism waits for elapse of a predetermined interval from the descent and only then allows passage of a signal, indicative of the missile flying over a target from the control, to a warhead-detonating fuze.

REFERENCES:
patent: 3831524 (1974-08-01), Pollin
patent: 3978797 (1976-09-01), Harrington et al.

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