Method for extending a nozzle and extended nozzle for rocket drives
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United States of America Patent
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Oct 30, 2007
Grant Date -
Nov 25, 2004
app pub date -
May 3, 2002
filing date -
May 15, 2001
priority date (Note) -
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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.
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