An improved model for the combustion of AP composite propellants
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8013
Reference16 articles.
1. A model of composite solid-propellant combustion based on multiple flames
2. 2Cohen, N.S. "Review of Composite Propellant Burn Rate Modeling,'M/>L4 Journal, Vol.18, March 1980, pp.277-293.
3. The combustion of solid monopropellants and composite propellants
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