2D model for unsteady burning heterogeneous AP/binder solid propellants
Author:
Affiliation:
1. Illinois, Univ., Urbana
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3573
Reference229 articles.
1. Burning Rate of Solid Propellant Ingredients, Part 2: Determination of Burning Rate Temperature Sensitivity
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