Method for extending a nozzle and extended nozzle for rocket...

Power plants – Reaction motor – Method of operation

Reexamination Certificate

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C060S771000, C239S265330

Reexamination Certificate

active

10477701

ABSTRACT:
A method for extending a nozzle for a rocket engine is described, in which at least one second region of the contour of the nozzle is arranged as an extension of a first region of the contour of the nozzle. This extension of the first region by the second region occurs at an altitude at which the contour of the open jet of the rocket engine substantially corresponds to the contour of the second region. Also described is a corresponding extendible nozzle for a rocket engine.

REFERENCES:
patent: 3394549 (1968-07-01), Sutor
patent: 4383407 (1983-05-01), Inman
patent: 4387564 (1983-06-01), Carey
patent: 4489889 (1984-12-01), Inman
patent: 4947644 (1990-08-01), Hermant
patent: 5282576 (1994-02-01), Chatenet et al.
patent: 6418710 (2002-07-01), Perrier et al.
patent: WO97/29277 (1997-08-01), None
G. Hagemann et al., “Advanced Rocket Nozzles”,J. of Propulsion and Power, 14(5), Sep.-Oct. 1998, pp. 620-634.
J. Beck et al., “Altitude Compensating Nozzles”, Rockwell Threshold, Summer 1995, pp. 38-44.
R. Schmucker, “Side loads and their reduction in liquid rocket engines”, Report TB-14, 24thInt'l Astronautical Congress, Baku, USSR, Oct. 7-13, 1973.

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