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| Research Progresses of Experiment, Mechanism, and Formulas of Low Vulnerable Propellants under Mechanical Stimulations |
| Received:February 06, 2019 Revised:March 29, 2019 |
| View Full Text View/Add Comment Download reader |
| DOI：10.7643/issn.1672-9242.2019.09.010 |
| KeyWord:low vulnerable propellant mechanical stimulation bullet impact, fragment impact shaped charge jet impact response mechanism |
| Author | Institution |
| LI Hai-tao |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
| WU Zhuo |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
| WANG Yue |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
| WANG Zheng |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
| LI Shang-wen |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
| HUANG Yin |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
| CHENG Hong-bo |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
| XU Shuang |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
| SONG Liu-fang |
Hubei Institute of Aerospace Chemical Technology, Xiangyang , China;Key Laboratory of Aerospace Chemical Power Technology, Xiangyang , China |
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| Abstract: |
| The theoretical and experimental researches of low vulnerable propellants in China are hysteretic compared with other countries, especially in the fields of bullet impact, fragment impact, and shaped charge jet impact, because they are limited by experimental conditions and assessment standard. To provide assistants for subsequent researches, progresses in three aspects were summarized in this review, including the experimental results of bullet impact, fragment impact, and shaped charge jet impact, the response mechanism of low vulnerable propellants suffering mechanical stimulations, and formulas researches of low vulnerable propellants. Some advices were provided finally to help the theoretic researches and industry productions in China. |
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