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Errata-Prediction of Burning Rates in Nozzleless Rocket Motors

✍ Scribed by King, Merrill K.

Book ID
121762103
Publisher
American Institute of Aeronautics and Astronautics
Year
1986
Tongue
English
Weight
138 KB
Volume
23
Category
Article
ISSN
0022-4650

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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