Effect of components on combustion properties of nitrate ester plasticized polyether

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

Effect of components on combustion properties of nitrate ester plasticized polyether

Yun Fei Liu^*, Huan Xiang Guan, Wei Shang Yao, Xiao Meng Li, 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

1 引用（Scopus）

摘要

Burning rate and burning rate-pressure exponent of nitrate ester plasticized polyethe propellant were studied by content and particle size of oxidizer AP, variety and content of burning rate catalysts, particle size of Al powder, modification of cross linking agent and processing aid. The results show that burning rate of the propellant can be regulated within 7.7-16.7 mm/s (7.0 MPa) and its static burning rate-pressure exponent can reach 0.50, while the minimum value is 0.41.

源语言	英语
页（从-至）	364-366
页数	3
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	26
期	4
出版状态	已出版 - 8月 2005

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title = "Effect of components on combustion properties of nitrate ester plasticized polyether",

abstract = "Burning rate and burning rate-pressure exponent of nitrate ester plasticized polyethe propellant were studied by content and particle size of oxidizer AP, variety and content of burning rate catalysts, particle size of Al powder, modification of cross linking agent and processing aid. The results show that burning rate of the propellant can be regulated within 7.7-16.7 mm/s (7.0 MPa) and its static burning rate-pressure exponent can reach 0.50, while the minimum value is 0.41.",

keywords = "Burning rate, Combustion performance, Pressure exponent, Solid propellant",

author = "Liu, {Yun Fei} and Guan, {Huan Xiang} and Yao, {Wei Shang} and Li, {Xiao Meng} and Tan, {Hui Min}",

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T1 - Effect of components on combustion properties of nitrate ester plasticized polyether

AU - Liu, Yun Fei

AU - Guan, Huan Xiang

AU - Yao, Wei Shang

AU - Li, Xiao Meng

AU - Tan, Hui Min

PY - 2005/8

Y1 - 2005/8

N2 - Burning rate and burning rate-pressure exponent of nitrate ester plasticized polyethe propellant were studied by content and particle size of oxidizer AP, variety and content of burning rate catalysts, particle size of Al powder, modification of cross linking agent and processing aid. The results show that burning rate of the propellant can be regulated within 7.7-16.7 mm/s (7.0 MPa) and its static burning rate-pressure exponent can reach 0.50, while the minimum value is 0.41.

AB - Burning rate and burning rate-pressure exponent of nitrate ester plasticized polyethe propellant were studied by content and particle size of oxidizer AP, variety and content of burning rate catalysts, particle size of Al powder, modification of cross linking agent and processing aid. The results show that burning rate of the propellant can be regulated within 7.7-16.7 mm/s (7.0 MPa) and its static burning rate-pressure exponent can reach 0.50, while the minimum value is 0.41.

KW - Burning rate

KW - Combustion performance

KW - Pressure exponent

KW - Solid propellant

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JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 4

ER -

Effect of components on combustion properties of nitrate ester plasticized polyether

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