Regulating system for guided missiles traveling at supersonic sp

Details Regulating system for guided missiles traveling at supersonic sp Regulating system for guided missiles traveling at supersonic sp

1984-11-05

1986-11-18

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

102384, F42B 1502, F42B 2524

Patent

active

046231072

ABSTRACT:
A regulating system for guided ammunition flying at supersonic speed, such as missiles, rockets, or projectiles which includes an arrangement for effecting the guidance through a partially changeable flow pressure. Provided on the ammunition are one or more steering systems in the form of ring-shaped or quasi-annular guidance mechanisms which are divided into sectors, and wherein the sectors cause a medium which become effective within the sectors to selectively and controllably block the airflow.

REFERENCES:
patent: 2495304 (1950-01-01), Wyckoff et al.
patent: 2584826 (1952-02-01), Wyckoff
patent: 3096739 (1963-07-01), Smith
patent: 3156207 (1964-11-01), Giles
patent: 3724782 (1973-04-01), Gauzza et al.

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