Analysis of Load Optimization in Solid Rocket Motor Propellant Grain with Pressure Cure
At present, the casting of large-size motors often adopts pressure cure. This technology can effectively reduce the risk of damage to the structural integrity of the grain in the case-bonded casting solid rocket motor. In this paper, ABAQUS is used to establish a finite element model of star-shaped...
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Main Authors: | Zhanxin Cui, Haiyang Li, Zhibin Shen, Huiru Cui |
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Format: | Article |
Language: | English |
Published: |
Wiley
2021-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2021/5026878 |
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