Research Progress on Structural Integrity of Solid Rocket Motor Grain

被引：0
|
作者：
Hou X. [1 ,2 ]
Zhang X. [2 ]
Liu X. [2 ]
Wu Y. [3 ]
Lei M. [4 ]
Wang X. [5 ]
Wang J. [2 ]
机构：
[1] China Aerospace Science and Technology Corporation, Beijing
[2] Beijing Institute of Technology, School of Aerospace Engineering, Beijing
[3] State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing
[4] School of Astronautics, Northwestern Polytechnical University, Xi'an
[5] Zhijian Lab, Rocket Force University of Engineering, Xi'an
来源：
Yuhang Xuebao/Journal of Astronautics | 2023年 / 44卷 / 04期
关键词：
Bonding interface; Propellant grain structure; Solid rocket motor; Structural integrity;
D O I：
10.3873/j.issn.1000-1328.2023.04.011
中图分类号：
学科分类号：
摘要：
A comprehensive review of the research progress in the structural integrity of solid rocket motor grain is presented, including mechanical properties of propellant and bonding interfaces, failure mechanisms, motor grain and propellant numerical simulation methods, and motor grain testing technology. The current trends or challenges in the studies about the structural integrity of solid rocket motor grain are also proposed. It is pointed out that in the future, the research direction and emphasis should be placed mainly on developing multi-scale characterizations and testing methods of propellants and bonding interfaces, advanced numerical simulation methods, comprehensive testing techniques for grains and eventually constructing an integrated evaluation platform. © 2023 China Spaceflight Society. All rights reserved.
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页码：566 / 579
页数：13
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