Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1973-06-18
1976-03-23
Engle, Samuel W.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42b 1500
Patent
active
039455882
ABSTRACT:
This invention which is a surface to surface anti-tank missile following a modified ballistic trajectory incorporating a guidance computer system with manual setting (ascending mode) and infrared optical system (descending mode), solid fuel rocket motor and a shaped charge high explosive warhead is designed as an effective and inexpensive means for the destruction of armored vehicles.
REFERENCES:
patent: 3504869 (1970-04-01), Evans et al.
patent: 3642233 (1972-02-01), Bezerie
Engle Samuel W.
Jordan C. T.
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