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A new look at AP/composite propellant combustion

Kumar, R. N. (1973) A new look at AP/composite propellant combustion. JPL Quarterly Technical Review, 3 (2). pp. 53-77. http://resolver.caltech.edu/CaltechAUTHORS:20101214-114320657

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Abstract

Some theoretical studies on the time-independent and oscillatory combustion of nonmetallized ammonium perchlorate (AP)/composite propellants are presented. A coherent and unified interpretation was made of the voluminous data available from experiments related to propellant combustion. Three fundamental hypotheses are introduced: the extent of propellant degradation at the vaporization step has to be specified through a scientific criterion; the condensed-phase degradation reaction of ammonium perchlorate to a vaporizable state is the overall rate-limiting step; gas-phase combustion rate is controlled by the mixing rate of fuel and oxidizer vapors. In the treatment of oscillatory combustion, the assumption of quasi-steady fluctuations in the gas phase is used to supplement these hypotheses.


Item Type:Article
Related URLs:
URLURL TypeDescription
http://ntrs.nasa.gov/index.jsp?method=order&oaiID=19730023133OrganizationUNSPECIFIED
Additional Information:© 1973. Unclassified; Copyright; Unlimited; Publicly available. JPL Quart. Tech. Rev., Vol. 3, No. 2 (NASA-CR-133863), p 45-77, Number of Pages = 25. Updated/Added to NTRS, 2006-08-02
Group:Guggenheim Jet Propulsion Center
Subject Keywords:chemistry, fluid mechanics, solid propulsion, thermodynamics
Other Numbering System:
Other Numbering System NameOther Numbering System ID
Guggenheim Jet Propulsion CenterUNSPECIFIED
NASACR-133863
Record Number:CaltechAUTHORS:20101214-114320657
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20101214-114320657
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:21356
Collection:CaltechAUTHORS
Deposited By: Ruth Sustaita
Deposited On:15 Dec 2010 22:13
Last Modified:26 Dec 2012 12:45

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