Study on the temperature effect in solid propellants under high-pressure waterjet impact

Hong Tao Yu; Yuan Hang He; Qing Ming Zhang

Study on the temperature effect in solid propellants under high-pressure waterjet impact

Hong Tao Yu^*, Yuan Hang He, Qing Ming Zhang

^*此作品的通讯作者

机电学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

7 引用（Scopus）

摘要

The ignition mechanism of solid propellants under high pressure waterjet remained unclear, so HTPB solid propellant of different formulas was used under high-pressure waterjet impact research. The results showed that during the process of impact of high-pressure waterjet with solid propellant the temperature of the samples increased significantly, and that the content of propellant components, ammonium perchlorate and ferrocene affected the heating rate significantly.

源语言	英语
页（从-至）	189-191
页数	3
期刊	Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
卷	28
期	3
出版状态	已出版 - 3月 2008

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引用此

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title = "Study on the temperature effect in solid propellants under high-pressure waterjet impact",

abstract = "The ignition mechanism of solid propellants under high pressure waterjet remained unclear, so HTPB solid propellant of different formulas was used under high-pressure waterjet impact research. The results showed that during the process of impact of high-pressure waterjet with solid propellant the temperature of the samples increased significantly, and that the content of propellant components, ammonium perchlorate and ferrocene affected the heating rate significantly.",

keywords = "Ammonium perchlorate (AP), Ferrocene, Solid propellant, Temperature effect, Waterjet",

author = "Yu, {Hong Tao} and He, {Yuan Hang} and Zhang, {Qing Ming}",

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AU - Yu, Hong Tao

AU - He, Yuan Hang

AU - Zhang, Qing Ming

PY - 2008/3

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N2 - The ignition mechanism of solid propellants under high pressure waterjet remained unclear, so HTPB solid propellant of different formulas was used under high-pressure waterjet impact research. The results showed that during the process of impact of high-pressure waterjet with solid propellant the temperature of the samples increased significantly, and that the content of propellant components, ammonium perchlorate and ferrocene affected the heating rate significantly.

AB - The ignition mechanism of solid propellants under high pressure waterjet remained unclear, so HTPB solid propellant of different formulas was used under high-pressure waterjet impact research. The results showed that during the process of impact of high-pressure waterjet with solid propellant the temperature of the samples increased significantly, and that the content of propellant components, ammonium perchlorate and ferrocene affected the heating rate significantly.

KW - Ammonium perchlorate (AP)

KW - Ferrocene

KW - Solid propellant

KW - Temperature effect

KW - Waterjet

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JO - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology

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ER -

Study on the temperature effect in solid propellants under high-pressure waterjet impact

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