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Effect of Diaphragms on Regression Rate in Hybrid Rocket Motors

✍ Scribed by Kumar, C. Palani; Kumar, Amit

Book ID
120531737
Publisher
American Institute of Aeronautics and Astronautics
Year
2013
Tongue
English
Weight
928 KB
Volume
29
Category
Article
ISSN
0748-4658

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## Abstract Through the analysis and calculation to the flow field in the solid rocket motor using high‐burning‐rate propellant, the authors believe that the existence of pressure difference between the inside and outside of the propellant tube causes the propellant crack. In this paper, the design