A Model of Erosive Burning of Composite Propellants
Author:
Affiliation:
1. Atlantic Research Corporation, Alexandria, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57298
Reference31 articles.
1. 2Viles, J.M. "Prediction of Rocket-Motor Chamber Pressures Using Measured Erosive-Burning Rates," Rohm and Haas Co., Huntsville, Ala. Technical Report S-275 (Contract DAAHO1-70-C0152, Oct. 1970.
2. Erosive burning- new experimental techniques and methods of analysis
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