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

^*Corresponding author for this work

School of Material Science and Engineering

Beijing Institute of Technology

Research output: Contribution to journal › Article › peer-review

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.

Original language	English
Pages (from-to)	50
Number of pages	1
Journal	Huozhayao Xuebao/Chinese Journal of Explosives and Propellants
Volume	26
Issue number	2
Publication status	Published - 2003

Keywords

Combustion property
NEPE propellant
Particle size

Cite this

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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.",

keywords = "Combustion property, NEPE propellant, Particle size",

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AU - Li, Xiao Meng

AU - Liu, Yun Fei

AU - Yao, Wei Shang

AU - Tan, Hui Min

PY - 2003

Y1 - 2003

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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M3 - Article

AN - SCOPUS:73849137584

SN - 1007-7812

VL - 26

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JO - Huozhayao Xuebao/Chinese Journal of Explosives and Propellants

JF - Huozhayao Xuebao/Chinese Journal of Explosives and Propellants

IS - 2

ER -

Study on combustion property of NEPE propellant with low aluminum content

Abstract

Keywords

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