Study on combustion property of NEPE propellant with low aluminum content

Xiao Meng Li; Yun Fei Liu; Wei Shang Yao; Hui Min Tan

Study on combustion property of NEPE propellant with low aluminum content

Xiao Meng Li^*, Yun Fei Liu, Wei Shang Yao, Hui Min Tan

^*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

摘要

The combustion properties of NEPE propellant with 8% aluminum content were studied. It was observed that increasing the ratio of NG/DEGDN, decreasing the particle size of AP, and increasing contents of fine particle AP are effective measures to increase the burning rates of the propellant. Simultaneously, decreasing the particle size of HMX can reduce it's burning rate and pressure exponent. PbCO₃ synthesized by ourselves can reduce the pressure exponent more than the bought one.

源语言	英语
页（从-至）	50
页数	1
期刊	Huozhayao Xuebao/Chinese Journal of Explosives and Propellants
卷	26
期	2
出版状态	已出版 - 2003

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引用此

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title = "Study on combustion property of NEPE propellant with low aluminum content",

abstract = "The combustion properties of NEPE propellant with 8% aluminum content were studied. It was observed that increasing the ratio of NG/DEGDN, decreasing the particle size of AP, and increasing contents of fine particle AP are effective measures to increase the burning rates of the propellant. Simultaneously, decreasing the particle size of HMX can reduce it's burning rate and pressure exponent. PbCO3 synthesized by ourselves can reduce the pressure exponent more than the bought one.",

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N2 - The combustion properties of NEPE propellant with 8% aluminum content were studied. It was observed that increasing the ratio of NG/DEGDN, decreasing the particle size of AP, and increasing contents of fine particle AP are effective measures to increase the burning rates of the propellant. Simultaneously, decreasing the particle size of HMX can reduce it's burning rate and pressure exponent. PbCO3 synthesized by ourselves can reduce the pressure exponent more than the bought one.

AB - The combustion properties of NEPE propellant with 8% aluminum content were studied. It was observed that increasing the ratio of NG/DEGDN, decreasing the particle size of AP, and increasing contents of fine particle AP are effective measures to increase the burning rates of the propellant. Simultaneously, decreasing the particle size of HMX can reduce it's burning rate and pressure exponent. PbCO3 synthesized by ourselves can reduce the pressure exponent more than the bought one.

KW - Combustion property

KW - NEPE propellant

KW - Particle size

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Study on combustion property of NEPE propellant with low aluminum content

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