Extendible nozzle

Power plants – Reaction motor – Including heat exchange means

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Details

2391271, F02K 984, F02K 152

Patent

active

050482890

ABSTRACT:
A thrust nozzle assembly for selective deployment and retraction of an extendible nozzle for a rocket engine.

REFERENCES:
patent: 3630449 (1971-12-01), Butler
patent: 4213566 (1980-07-01), Miltenberger
patent: 4245469 (1981-01-01), Fortini et al.
patent: 4313567 (1982-02-01), Feight
patent: 4489889 (1984-12-01), Inman
patent: 4779799 (1988-10-01), Jancer
patent: 4909032 (1990-03-01), Horiuchi et al.

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