Thrust control nozzle for rockets

Details Thrust control nozzle for rockets Thrust control nozzle for rockets

1971-09-13

1979-09-18

Love, John J.

Fluid sprinkling, spraying, and diffusing

Reaction motor discharge nozzle

With means controlling amount, shape or direction of...

23926535, B63H 1110

Patent

active

041680316

ABSTRACT:
The cowl of a spike nozzle is attached to the inside of the aft closure of a rocket case by means that allow it to rotate about a fixed point. Fluid-operated actuators mounted in the aft closure bear against the cowl to effect changes in the direction of thrust. Optionally, the spike may be attached to its cowl by fluid-operated actuators to modulate thrust.

REFERENCES:
patent: 2857119 (1958-10-01), Morguloff
patent: 2987879 (1961-06-01), Brown
patent: 3096616 (1963-07-01), Edman
patent: 3130544 (1964-04-01), Penza
patent: 3332243 (1967-06-01), Wilson
patent: 3358453 (1967-12-01), Swet
patent: 3392918 (1968-07-01), Goldberg
patent: 3402894 (1968-09-01), Wynosky et al.
patent: 3504902 (1970-04-01), Irwin
patent: 3659789 (1972-05-01), Schultz
patent: 3727843 (1973-04-01), Parilla

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