Combustion characteristics of AP/HTPB propellants with burning rate modifiers
- 1 July 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 8 (4) , 748-755
- https://doi.org/10.2514/3.23545
Abstract
No abstract availableKeywords
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