Analytical model of the combustion of multicomponent solid propellants-Reference-Cited by-同舟云学术

Analytical model of the combustion of multicomponent solid propellants

Published:1977-07-11 Issue: Volume: Page:
ISSN:
Container-title:13th Propulsion Conference
language:
Short-container-title:

Author:

COHEN N.¹,PRICE C.¹,STRAND L.¹

Affiliation:

1. California Institute of Technology, Jet Propulsion Laboratory, Pasadena, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1977-927

Reference29 articles.

1. A model of composite solid-propellant combustion based on multiple flames

2. Hamann, R. J. "Three Solid Propellant Combustion Models, a Comparison and Some Applications to Non-Steady Cases," Ph.D. Thesis,Delft University of Technology, Na. M-215,April 1974, The Netherlands.

3. McCarty, K. P., Beckstead, M. W. and Simmons, R. L. "HMX Propellant Combustion Studies," Report AFRPL-TR-76-59. Dec. 1976, Hercules Inc., Magna. Utah; AFRPL (STINFO)/DOX, Edwards AFB,California.

4. Derr. R. L. Beckstead, M. W. and Cohen, N. S. "Combustion Tailoring Criteria for Solid Propellants," Report AFRPL-TR-69-190, May 1969, Lockheed Propulsion Co. (defunct), Redlands, California; AFRPL (STINFO)/WZ, Edwards AFB,California.

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