A model of composite solid-propellant combustion based on multiple flames
Author:
Affiliation:
1. Lockheed Propulsion Company, Redlands, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6087
Reference31 articles.
1. Burning Mechanism of Ammonium Perchlorate Propellants
2. ARS Progress in Astronautics and Rocketry;Chaiken R. F.,1960
3. ARS Progress in Astronautics and Rocketry;Nachbar W.,1960
4. A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat Generation
5. A DETAILED MODEL OF THE COMBUSTION OF COMPOSITE SOLID PROPELLANTS
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