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Fracture of a burning solid propellant attenuated by a crack-type cavity

✍ Scribed by V. M. Mirsalimov; B. É. Rustamov


Book ID
110169905
Publisher
SP MAIK Nauka/Interperiodica
Year
2011
Tongue
English
Weight
160 KB
Volume
52
Category
Article
ISSN
0021-8944

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Research on the Crack Mechanism of High-
✍ D. A. Wang; N. F. Wang; G. M. Qin 📂 Article 📅 1995 🏛 John Wiley and Sons 🌐 English ⚖ 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