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The effect of cross-flow temperature on the burning rate in a solid propellant

✍ Scribed by Atsushi Ishihara

Book ID
108392585
Publisher
Elsevier Science
Year
1992
Tongue
English
Weight
495 KB
Volume
24
Category
Article
ISSN
1540-7489

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Research on the Crack Mechanism of High-
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✍ D. A. Wang; N. F. Wang; G. M. Qin πŸ“‚ Article πŸ“… 1995 πŸ› John Wiley and Sons 🌐 English βš– 406 KB

## 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