Energy characteristics computation of propellant containing 3,3'-dinitro-4,4'-oxazafurazan

Xu Peng Wang; Yun Jun Luo; Kai Guo; Yong Lv

Energy characteristics computation of propellant containing 3,3'-dinitro-4,4'-oxazafurazan

Xu Peng Wang^*, Yun Jun Luo, Kai Guo, Yong Lv

^*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

9 引用（Scopus）

摘要

The energy parameters of the propellant containing 3,3'-dinitro-4,4'-oxazafurazan (DNOAF) were calculated under standard condition(p_c/p_o=70:1). Replacing ammonium perchlorate(AP) with DNOAF in HTPB propellant increases the specific impulse for 120 N · s · kg^-1, and NC/NG/DNOAF smokeless CMDB propellant has a specific impulse of 2558 N · s · kg^-1, and replacing HMX with DNOAF in PET/NG/DEGDN/HMX propellant increases the specific impulse for 194 N · s · kg^-1.

源语言	英语
页（从-至）	79-82
页数	4
期刊	Hanneng Cailiao/Chinese Journal of Energetic Materials
卷	17
期	1
出版状态	已出版 - 2月 2009

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title = "Energy characteristics computation of propellant containing 3,3'-dinitro-4,4'-oxazafurazan",

abstract = "The energy parameters of the propellant containing 3,3'-dinitro-4,4'-oxazafurazan (DNOAF) were calculated under standard condition(pc/po=70:1). Replacing ammonium perchlorate(AP) with DNOAF in HTPB propellant increases the specific impulse for 120 N · s · kg-1, and NC/NG/DNOAF smokeless CMDB propellant has a specific impulse of 2558 N · s · kg-1, and replacing HMX with DNOAF in PET/NG/DEGDN/HMX propellant increases the specific impulse for 194 N · s · kg-1.",

keywords = "Energy characteristics, Furazan, High energy propellant, Oxidizer, Physical chemistry, Smokeless propellant",

author = "Wang, {Xu Peng} and Luo, {Yun Jun} and Kai Guo and Yong Lv",

year = "2009",

month = feb,

language = "English",

volume = "17",

pages = "79--82",

journal = "Hanneng Cailiao/Chinese Journal of Energetic Materials",

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T1 - Energy characteristics computation of propellant containing 3,3'-dinitro-4,4'-oxazafurazan

AU - Wang, Xu Peng

AU - Luo, Yun Jun

AU - Guo, Kai

AU - Lv, Yong

PY - 2009/2

Y1 - 2009/2

N2 - The energy parameters of the propellant containing 3,3'-dinitro-4,4'-oxazafurazan (DNOAF) were calculated under standard condition(pc/po=70:1). Replacing ammonium perchlorate(AP) with DNOAF in HTPB propellant increases the specific impulse for 120 N · s · kg-1, and NC/NG/DNOAF smokeless CMDB propellant has a specific impulse of 2558 N · s · kg-1, and replacing HMX with DNOAF in PET/NG/DEGDN/HMX propellant increases the specific impulse for 194 N · s · kg-1.

AB - The energy parameters of the propellant containing 3,3'-dinitro-4,4'-oxazafurazan (DNOAF) were calculated under standard condition(pc/po=70:1). Replacing ammonium perchlorate(AP) with DNOAF in HTPB propellant increases the specific impulse for 120 N · s · kg-1, and NC/NG/DNOAF smokeless CMDB propellant has a specific impulse of 2558 N · s · kg-1, and replacing HMX with DNOAF in PET/NG/DEGDN/HMX propellant increases the specific impulse for 194 N · s · kg-1.

KW - Energy characteristics

KW - Furazan

KW - High energy propellant

KW - Oxidizer

KW - Physical chemistry

KW - Smokeless propellant

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AN - SCOPUS:62749128563

SN - 1006-9941

VL - 17

SP - 79

EP - 82

JO - Hanneng Cailiao/Chinese Journal of Energetic Materials

JF - Hanneng Cailiao/Chinese Journal of Energetic Materials

IS - 1

ER -

Energy characteristics computation of propellant containing 3,3'-dinitro-4,4'-oxazafurazan

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