A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat Generation
Author:
Affiliation:
1. University of Waterloo, Waterloo, Ontario, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.55284
Reference19 articles.
1. Nachbar, W.UA theoretical study of the burning of a solid propellant sandwich," ARS Progress in Astronautics and Rocketry: Solid Propellant Rocket Research, edited by M. Summerfield (Academic Press Inc., New York,1960), Vol.I, pp.207-226.
2. Burning Mechanism of Ammonium Perchlorate Propellants
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