Temperature sensitivity coefficients of solid propellant burning rate
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference11 articles.
1. Relationships among solid propellant temperature sensitivity parameters;Brooks,1981
2. Oxidizer size distribution effects on propellant combustion;Renie;AIAA J.,1979
3. A model of composite solid-propellant combustion based on multiple flames;Beckstead;AIAA J.,1970
4. The correlation of interior ballistics data for solid propellants;Geckler;Jet Propulsion,1954
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