A MODEL FOR SOLID PROPELLANT COMBUSTION 179 data generated by Shannon~ for pressed AP strands. Combustion of Solid Propellants G. Lengellé, J. Duterque, J.F. The BDP model and other derivative models have all incorporated the same idea and form of equation which is dependent on pressure.
American Institute of Aeronautics and Astronautics 12700 Sunrise Valley Drive, Suite 200 Reston, VA 20191-5807 703.264.7500 Considering tran- sient heat transfer equations, it is apparent that burn rate should be an independent variable rather than pressure.
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