In-flight reconfigurable missile construction

Details In-flight reconfigurable missile construction In-flight reconfigurable missile construction

1989-03-27

1991-04-09

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Externally mounted stabilizing appendage

F42B 1012

Patent

active

050057812

ABSTRACT:
A staged missile which is reconfigured in-flight solely by changing vehicle dynamics enabling packaging of kinetric energy kill capability in severely constrained envelopes, thus retaining the use of existing tactical assets to counter advanced armored threats.

REFERENCES:
patent: 1257126 (1918-02-01), Schneider
patent: 2344957 (1944-03-01), Anzalone
patent: 3125957 (1964-03-01), Lipinski
patent: 3167016 (1965-01-01), Czerwinski
patent: 3377952 (1968-04-01), Crockett
patent: 3491692 (1970-01-01), Blankenagel
patent: 3601055 (1971-08-01), Crockett
patent: 4708304 (1987-11-01), Wederetz et al.

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