Study on decreasing the burning rate of nitrate ester plasticized polyether propellant

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

Study on decreasing the burning rate of nitrate ester plasticized polyether propellant

Huan Xiang Guan^*
, Yun Fei Liu
, Wei Shang Yao
, Hui Min Tan

^*此作品的通讯作者

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

8 引用（Scopus）

摘要

Reducing burning rate of nitrate ester plasticized polyether (NEPE) propellant was studied by means of adding some burning rate modifiers and adjusting its composition. The results show that burning rate of the propellant can be depressed by enlarging the particle size of AP, reducing the ratio of NG/DEGDN, decreasing the content of AP and adding little content of burning rate modifiers. The burning rate under 7.0 MPa can be reduced to 6.87 mm/s with ratio 1:1:1 of burning rate modifiers glycerol triacetate/polyoxymethylene/sucrose octa-acetate.

源语言	英语
页（从-至）	216-219
页数	4
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	28
期	2
出版状态	已出版 - 5月 2007
已对外发布	是

其它文件与链接

链接到 Scopus 的出版物

引用此

@article{99a50655729e4813a3b7089f8914e461,

title = "Study on decreasing the burning rate of nitrate ester plasticized polyether propellant",

abstract = "Reducing burning rate of nitrate ester plasticized polyether (NEPE) propellant was studied by means of adding some burning rate modifiers and adjusting its composition. The results show that burning rate of the propellant can be depressed by enlarging the particle size of AP, reducing the ratio of NG/DEGDN, decreasing the content of AP and adding little content of burning rate modifiers. The burning rate under 7.0 MPa can be reduced to 6.87 mm/s with ratio 1:1:1 of burning rate modifiers glycerol triacetate/polyoxymethylene/sucrose octa-acetate.",

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

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

year = "2007",

month = may,

language = "English",

volume = "28",

pages = "216--219",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "Journal of Propulsion Technology",

number = "2",

}

TY - JOUR

T1 - Study on decreasing the burning rate of nitrate ester plasticized polyether propellant

AU - Guan, Huan Xiang

AU - Liu, Yun Fei

AU - Yao, Wei Shang

AU - Tan, Hui Min

PY - 2007/5

Y1 - 2007/5

N2 - Reducing burning rate of nitrate ester plasticized polyether (NEPE) propellant was studied by means of adding some burning rate modifiers and adjusting its composition. The results show that burning rate of the propellant can be depressed by enlarging the particle size of AP, reducing the ratio of NG/DEGDN, decreasing the content of AP and adding little content of burning rate modifiers. The burning rate under 7.0 MPa can be reduced to 6.87 mm/s with ratio 1:1:1 of burning rate modifiers glycerol triacetate/polyoxymethylene/sucrose octa-acetate.

AB - Reducing burning rate of nitrate ester plasticized polyether (NEPE) propellant was studied by means of adding some burning rate modifiers and adjusting its composition. The results show that burning rate of the propellant can be depressed by enlarging the particle size of AP, reducing the ratio of NG/DEGDN, decreasing the content of AP and adding little content of burning rate modifiers. The burning rate under 7.0 MPa can be reduced to 6.87 mm/s with ratio 1:1:1 of burning rate modifiers glycerol triacetate/polyoxymethylene/sucrose octa-acetate.

KW - Burning rate modifiers

KW - Combustion performance

KW - Pressure exponent

KW - Solid propellant

UR - https://www.scopus.com/pages/publications/34250357938

M3 - Article

AN - SCOPUS:34250357938

SN - 1001-4055

VL - 28

SP - 216

EP - 219

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 2

ER -

Study on decreasing the burning rate of nitrate ester plasticized polyether propellant

摘要

其它文件与链接

学术指纹

引用此