Analytical Solution for Pressure-Coupled Combustion Response Functions of Composite Solid Propellants
Author:
Affiliation:
1. California Institute of Technology, Pasadena, California 91125
2. Cohen Professional Services, Los Angeles, California 90035
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/10.2514/1.21502
Reference16 articles.
1. A review of calculations for unsteady burning of a solid propellant.
2. Combustion of ammonium perchlorate-polymer sandwiches
3. An improved model for the combustion of AP composite propellants
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