Propellant Combustion Instability as Measured by Combustion Recoil
Author:
Affiliation:
1. Thiokol/Wasatch Chemical Corporation, Brigham City, Utah
2. University of Utah, Salt Lake City, Utah
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50372
Reference16 articles.
1. Effect of surface reactions on acoustic response of solid propellants.
2. An Elementary Calculation for the Burning Rate of Composite Solid Propellants
3. A Simplified Model of Unstable Burning in Solid Propellants
4. Effect of surface reactions on the solid propellant response function.
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