Missile system with acceleration induced operational energy

Details Missile system with acceleration induced operational energy Missile system with acceleration induced operational energy

1981-01-12

1983-11-15

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

102207, F42B 1500, F41G 722

Patent

active

044151306

ABSTRACT:
A missile system is disclosed which collects and stores energy during the early stages of flight of a missile at a time when the acceleration forces on the missile are the greatest and thereafter, regulates the stored energy to at least one mechanism on board the missile for operation thereof. More specifically, the missile system includes a main support housing section and a nose cone section which is slidably, mechanically interconnected to the housing section. During the early stages of flight, the nose cone section is caused to move with respect to the housing section under the induced acceleration of the missile. Means are provided on board the missile to collect and store the energy resulting from the acceleration induced movement of the nose cone section with respect to the housing section and to provide the stored energy in a regulated fashion to at least one mechanism disposed on the missile for operation thereof during the flight time of the missile.

REFERENCES:
patent: 3081051 (1963-03-01), Robinson, Jr.
patent: 3111088 (1963-11-01), Fisk
patent: 3324317 (1967-06-01), Hazelet
patent: 3843075 (1974-10-01), Weber et al.
patent: 4193567 (1980-03-01), McCarty, Jr.

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