Test-Based Thermal Decomposition Simulation of AP/HTPB and AP/HTPE Propellants
Author:
Affiliation:
1. Seoul National University, Seoul 151-744, Korea
2. Agency for Defense Development, Daejeon 305-600, Korea
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/10.2514/1.B34099
Reference13 articles.
1. Thermal decomposition of ammonium perchlorate
2. Thermal Decomposition of AMMO/AP Composite Propellants
3. The mechanism of burning rate catalysis in composite HTPBAP propellant combustion
4. Modeling of combustion and ignition of solid-propellant ingredients
5. A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat Generation
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