Adjustable rocket thrust alignment device

Aeronautics and astronautics – Miscellaneous

Patent

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Details

73 65, 244 54, 244 55, B64D 4700, B64F 500

Patent

active

044456522

ABSTRACT:
An alignment device for adjusting the takeoff assist thrust vector of a rocket booster in a desired relationship to the center of gravity of an autonomous missile. The device provides for using "plumb bob type" hanging tool prior to installing the rocket booster on the missile.

REFERENCES:
patent: 2391243 (1945-12-01), Hutton
patent: 2946285 (1960-07-01), Nauschutz
patent: 3174330 (1965-03-01), Boundy
patent: 3278138 (1966-10-01), Haberkorn
patent: 3349566 (1967-10-01), Tyrrell et al.
patent: 3897030 (1975-07-01), Cors et al.

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