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Role of Condensed Phase Details in the Oscillatory Combustion of Composite Propellants

Kumar, R. N. and Culick, F. E. C. (1977) Role of Condensed Phase Details in the Oscillatory Combustion of Composite Propellants. Combustion Science and Technology, 15 (5). pp. 179-199. ISSN 0010-2202. doi:10.1080/00102207708946783.

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The response functions of composite propellants are theoretically derived, including explicitly the pressure-dependent degradation term in the condensed phase, hypothesizing that the overall rate-limiting reactions are in the relatively low temperature condensed phase. The method of "inner" and "outer" expansions with the reduced activation energy as the singular perturbation parameter has been employed. The results cover subsurface reactions with and without surface reactions, adiabatic and uniform-combustion models for the quasisteady gas phase processes. The response functions display several experimentally observed features like dependence on mean pressure and the instability behavior of some "zero-n" propellants.

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Additional Information:© Gordon and Breach Science Publishers Ltd., 1977. Received September 28, 1976; in final form December 7, 1976. This work was performed for JPL (NASA Contract NAS 7-100) under the Work Order 61496. The authors thank Mr. Warren Dowler for helpful discussions and his enthusiastic encouragement at all stages.
Group:Guggenheim Jet Propulsion Center, GALCIT
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Other Numbering System NameOther Numbering System ID
Guggenheim Jet Propulsion CenterUNSPECIFIED
NASA Work Order61496
Issue or Number:5
Record Number:CaltechAUTHORS:20101213-105529799
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Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:21316
Deposited By: Ruth Sustaita
Deposited On:14 Dec 2010 16:56
Last Modified:09 Nov 2021 00:07

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