An interceptor missile has a single gimbal system mounted in its interior. The single gimbal system positions a directional warhead carried by the missile to provide the maximum destructive effect upon detonation to an air supported target. This invention generally relates to a fragmentation warhead fuze system for medium range interceptor missiles and rockets which are intended for deployment against air supported targets, and more particularly to an improved non-nuclear warhead fuze seeker system for such missiles and rockets.
Warhead Fuze Seeker
1965
4 pages
Report
Keine Angabe
Englisch
NTIS | 1971
|British Library Conference Proceedings | 2013
|Online Contents | 1993
|NTIS | 1976
|TIBKAT | 1983
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