固体发动机低易损性评估研究进展

Jun Li; Qingjie Jiao; Aimin Pang; Hui Ren; Jianxin Nie; Liguo Cheng; Jing Su; Hongbo Guan; Xu Xiao; Jiefan Zhang

doi:10.7673/j.issn.1006-2793.2019.01.001

固体发动机低易损性评估研究进展

Jun Li, Qingjie Jiao, Aimin Pang, Hui Ren, Jianxin Nie, Liguo Cheng, Jing Su, Hongbo Guan, Xu Xiao, Jiefan Zhang

机电学院

科研成果: 期刊稿件 › 文章 › 同行评审

7 引用（Scopus）

摘要

In order to establish the test method and evaluation procedure for low-vulnerability properties of solid rocket motor,this paper mainly discusses the effects of sample sizes and constraints on the test results,on the basis of current states of reported design of rocket motors.The test method and evaluation procedure are verified by experiments on the full-scale solid rocket motors,which may provide reference for formulation design of solid rocket motor.

投稿的翻译标题	Recent progress on evaluation of low-vulnerability properties for solid rocket motor
源语言	繁体中文
页（从-至）	1-6 and 15
期刊	Guti Huojian Jishu/Journal of Solid Rocket Technology
卷	42
期	1
DOI	https://doi.org/10.7673/j.issn.1006-2793.2019.01.001
出版状态	已出版 - 1 2月 2019

关键词

Evaluation method
Low-vulnerability properties
Solid rocket motor

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10.7673/j.issn.1006-2793.2019.01.001

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引用此

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AU - Li, Jun

AU - Jiao, Qingjie

AU - Pang, Aimin

AU - Ren, Hui

AU - Nie, Jianxin

AU - Cheng, Liguo

AU - Su, Jing

AU - Guan, Hongbo

AU - Xiao, Xu

AU - Zhang, Jiefan

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N2 - In order to establish the test method and evaluation procedure for low-vulnerability properties of solid rocket motor,this paper mainly discusses the effects of sample sizes and constraints on the test results,on the basis of current states of reported design of rocket motors.The test method and evaluation procedure are verified by experiments on the full-scale solid rocket motors,which may provide reference for formulation design of solid rocket motor.

AB - In order to establish the test method and evaluation procedure for low-vulnerability properties of solid rocket motor,this paper mainly discusses the effects of sample sizes and constraints on the test results,on the basis of current states of reported design of rocket motors.The test method and evaluation procedure are verified by experiments on the full-scale solid rocket motors,which may provide reference for formulation design of solid rocket motor.

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KW - Low-vulnerability properties

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IS - 1

ER -

固体发动机低易损性评估研究进展

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关键词

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