Control after burnout for reaction steered missiles

Details Control after burnout for reaction steered missiles Control after burnout for reaction steered missiles

1974-08-15

1978-03-14

Pendegrass, Verlin R.

Ammunition and explosives

Igniting devices and systems

244 322, 149 1991, 149 92, F42B 1330, C06C 2534

Patent

active

040784959

ABSTRACT:
The warhead of a missile is loaded with a payload that can either be burned r exploded. If propulsion is lost and either aerodynamic steering is not present or the velocity level of the missile is degraded to a point where steering is marginal, steerage is maintained by igniting the warhead payload and exhausting gases through nozzles attached to the warhead.

REFERENCES:
patent: 2822755 (1958-02-01), Edwards et al.
patent: 3138501 (1964-06-01), Wright
patent: 3490373 (1970-01-01), Fox
patent: 3572249 (1971-03-01), Davis
patent: 3756874 (1973-09-01), Chang et al.

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