Structural Integrity Analyses on the Anti-high Overload of a Solid Rocket Motor
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-031-42515-8_30
Reference12 articles.
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3. Chyuan, S.W.: Numerical study of solid propellant grains subjected to unsteady state thermal loading. Int. J. Comput. Appl. Technol. 24(2), 98–109 (2005)
4. Chyuan, S.W.: Dynamic analysis of solid propellant grains subjected to ignition pressurization loading. J. Sound Vib. 268(3), 465–483 (2003)
5. Ma, W., Wang, N., Sui, X., Li, S., Xie, K.: Thermal safety of a gun-launched missile’s solid rocket motor under conditions of high environm. Temp. and overloaded forces. Propell. Explos. Pyrotech. 43(12), 0721–3115 (2018)
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