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New Method to Determine the Velocities of Particles on a Solid Propellant Surface in a Solid Rocket Motor

✍ Scribed by Xiao, Yumin; Amano, R. S.; Cai, Timin; Li, Jiang


Book ID
121796551
Publisher
The American Society of Mechanical Engineers
Year
2005
Tongue
English
Weight
239 KB
Volume
127
Category
Article
ISSN
0022-1481

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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