Combustion wave structures of ammonium perchlorate composite propellants
Author:
Affiliation:
1. Japan Defense Agency, Tachikawa, Tokyo, Japan
2. Nissan Motor Co., Ltd., Suginami, Tokyo, Japan
3. Nippon Oil and Fats Co., Ltd., Taketoyo, Aichi, Japan
4. Daicel Chemical Industries, Ltd., Ibogawa, Hyogo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.22885
Reference9 articles.
1. 2Bastress, E. K. "Modification of the Burning Rates of Ammonium Perchlorate Solid Propellants by Particle Size Control," Ph.D. Thesis,Department of Aeronautical Engineering, Princeton University, Princeton, NJ,Jan., 1961.
2. A model of composite solid-propellant combustion based on multiple flames
3. A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat Generation
4. Physicochemical processes of HMX propellant combustion
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