Linear pyrolysis rate measurements of propellant constituents
Author:
Affiliation:
1. Lockheed Propulsion Company, Redlands, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3118
Reference15 articles.
1. The An Hypothesis for Propellant Burning.
2. McClure, F. T., Hart, R. W., and Bird, J. F. "Solid propellant rocket motors as acoustic oscillators," Solid Propellant Rocket Research (Academic Press, London, 1960), pp.295-358.
3. A Simplified Model of Unstable Burning in Solid Propellants
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