A kinetic model for the premixed combustion of a fine AP/HTPB composite propellant-Reference-Cited by-同舟云学术

A kinetic model for the premixed combustion of a fine AP/HTPB composite propellant

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Jeppson M.¹,Beckstead M.²,Jing Q.³

Affiliation:

1. Grumman Aerospace Corp., Bethpage, NY

2. UNITED AIRCRAFT CORP., PRATT ANDWHITNEY AIRCRAFT DIV., EAST HARTFORD, CONN.

3. WATERLOO, U., WATERLOO, ONTARIO, CANADA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-447

Reference30 articles.

1. Beckstead, M.W."Solid Propellant Combustion Mechanisms and FlameStructure,"Pure &Applied Chemistry, (1993),Vol. 65, No.2,pp. 297-307.

2. Korobeinichev, O.P.,N.E. Ermolin, A.A.Chernov, and I.D. Emel'yanov, "Flame Structure, Kinetics and Mechanism of Chemical Reactions in Flames of Mixed Composition Based on Ammonium Perchlorate and Polybutadiene Rubber," Combustion, Explosion, and Shock Waves,(1992),Vol.28,No.4,pp.53-59.

3. Manelis,G.B.and V.A.Strunin, "TheMechanismof Ammonium PerchlorateBurning,"Combustionand Flame,(1971),No. 17, pp.69-77.

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