Dual purpose guidance system for a guided missile

Communications: directive radio wave systems and devices (e.g. – Return signal controls external device – Missile or spacecraft guidance

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Details

102214, 244 319, 342 68, F42B 1502, F42C 1304

Patent

active

046300503

ABSTRACT:
A guided missile having a radar system which is utilized as a target seeker and tracking radar as long as it is capable of tracking the target through the encounter, after which, or at some set distance from the target, the radar and associated circuitry provides the optimum burst time.

REFERENCES:
patent: 3698811 (1972-10-01), Weil
patent: 4100545 (1978-07-01), Tabourier
patent: 4160974 (1979-07-01), Stavis
patent: 4256275 (1981-03-01), Flick et al.
patent: 4321871 (1982-03-01), Abadie

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