Burning Rate Characteristics of Ammonium Perchloarte-Based Composite Propellant Using Bimodal Ammonium Perchlorate
- 1 May 2008
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 24 (3), 499-506
- https://doi.org/10.2514/1.27107
Abstract
No abstract availableKeywords
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