Jet tab steerable missile

Details Jet tab steerable missile Jet tab steerable missile

1974-03-27

1976-10-19

Pendegrass, Verlin R.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

244 322, 23926519, F42B 1502

Patent

active

039866831

ABSTRACT:
A jet tab steerable missile having a plurality of tab-shaped elements rotatably mounted on the rear portion of the missile adjacent the nozzle. The tab-shaped elements are capable of 360.degree. rotary movement from a thrust vector control position into the air stream. In so doing the tab-shaped elements will provide post "burn out" side force generation, and therefore, extend range control of the missile.

REFERENCES:
patent: 2692475 (1954-10-01), Hull
patent: 2850977 (1958-09-01), Pollak
patent: 2879955 (1959-03-01), Zborowski
patent: 2969017 (1961-01-01), Kershner
patent: 3188958 (1965-06-01), Burke et al.
patent: 3205820 (1965-09-01), McCorkle, Jr. et al.
patent: 3384325 (1968-05-01), Hermann

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