Reducing apparent burning rate pressure exponent of ultra high burning rate propellant

Xiao Dong Li; Rong Jie Yang; Jian Min Li; Ji Yu He

Reducing apparent burning rate pressure exponent of ultra high burning rate propellant

Xiao Dong Li^*, Rong Jie Yang, Jian Min Li, Ji Yu He

^*此作品的通讯作者

材料学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

The characteristic burning rate (u)-pressure (p) curves of ultrahigh burning rate propellant (UHBRP) were analyzed theoretically. A technological method to reduce the apparent burning rate pressure exponent of UHBRP was used in preparation of UHBRP pellets. A large volume closed bomb was used to measure the burning rates of the UHBRP samples. The u-p curves of UHBRP of density gradient show the plateau combustion characteristics.

源语言	英语
页（从-至）	422-425
页数	4
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	22
期	5
出版状态	已出版 - 10月 2001

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Li, X. D., Yang, R. J., Li, J. M., & He, J. Y. (2001). Reducing apparent burning rate pressure exponent of ultra high burning rate propellant. Tuijin Jishu/Journal of Propulsion Technology, 22(5), 422-425.

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abstract = "The characteristic burning rate (u)-pressure (p) curves of ultrahigh burning rate propellant (UHBRP) were analyzed theoretically. A technological method to reduce the apparent burning rate pressure exponent of UHBRP was used in preparation of UHBRP pellets. A large volume closed bomb was used to measure the burning rates of the UHBRP samples. The u-p curves of UHBRP of density gradient show the plateau combustion characteristics.",

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KW - Mesa-burning propellant

KW - Pressure exponent

KW - Propellant combustion

KW - Superhigh burning rate propellant

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Reducing apparent burning rate pressure exponent of ultra high burning rate propellant

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