Difference between revisions of "Auxiliary Fluid Ignition"
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Latest revision as of 16:00, 30 March 2007
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Auxiliary Fluid Ignition
A method of ignition of a liquid-propellant
rocket engine
in which a liquid which is
hypergolic with either the
fuel or the
oxidizer is injected into the combustion
chamber to initiate combustion.
Aniline is used as an auxiliary fluid with nitric acid
and some organic fuels to initiate combustion.
References
This article is based on NASA's Dictionary of Technical Terms for Aerospace Use
