Energy characteristics computation of propellant containing octanitrocubane (ONC)

Jing Ru Liu; Yun Jun Luo; Yin Yang

Energy characteristics computation of propellant containing octanitrocubane (ONC)

Jing Ru Liu^*, Yun Jun Luo, Yin Yang

^*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

3 引用（Scopus）

摘要

The energy parameters of the propellant containing octanitrocubane (ONC) are calculated by CAD system of propellant energy calculation under standard condition (p_c/p_o=70:1). Replacing ammonium perchlorate with octanitrocubane in HTPB propellant increases the specific impulse for 125 N·s·kg^-1, NC/NG/ONC smokeless MDB propellant has a specific impulse of 2545 N·s·kg^-1, GAP/ONC/RDX smokeless propellant has a high specific impulse over 2600 N·s·kg^-1 in very wide scope.

源语言	英语
页（从-至）	367-369
页数	3
期刊	Hanneng Cailiao/Chinese Journal of Energetic Materials
卷	15
期	4
出版状态	已出版 - 8月 2007

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title = "Energy characteristics computation of propellant containing octanitrocubane (ONC)",

abstract = "The energy parameters of the propellant containing octanitrocubane (ONC) are calculated by CAD system of propellant energy calculation under standard condition (pc/po=70:1). Replacing ammonium perchlorate with octanitrocubane in HTPB propellant increases the specific impulse for 125 N·s·kg-1, NC/NG/ONC smokeless MDB propellant has a specific impulse of 2545 N·s·kg-1, GAP/ONC/RDX smokeless propellant has a high specific impulse over 2600 N·s·kg-1 in very wide scope.",

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

author = "Liu, {Jing Ru} and Luo, {Yun Jun} and Yin Yang",

year = "2007",

month = aug,

language = "English",

volume = "15",

pages = "367--369",

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

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AU - Liu, Jing Ru

AU - Luo, Yun Jun

AU - Yang, Yin

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N2 - The energy parameters of the propellant containing octanitrocubane (ONC) are calculated by CAD system of propellant energy calculation under standard condition (pc/po=70:1). Replacing ammonium perchlorate with octanitrocubane in HTPB propellant increases the specific impulse for 125 N·s·kg-1, NC/NG/ONC smokeless MDB propellant has a specific impulse of 2545 N·s·kg-1, GAP/ONC/RDX smokeless propellant has a high specific impulse over 2600 N·s·kg-1 in very wide scope.

AB - The energy parameters of the propellant containing octanitrocubane (ONC) are calculated by CAD system of propellant energy calculation under standard condition (pc/po=70:1). Replacing ammonium perchlorate with octanitrocubane in HTPB propellant increases the specific impulse for 125 N·s·kg-1, NC/NG/ONC smokeless MDB propellant has a specific impulse of 2545 N·s·kg-1, GAP/ONC/RDX smokeless propellant has a high specific impulse over 2600 N·s·kg-1 in very wide scope.

KW - Energy characteristics

KW - High energy propellant

KW - Otanitrocubane

KW - Oxidizer

KW - Physical chemistry

KW - Smokeless propellant

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JO - Hanneng Cailiao/Chinese Journal of Energetic Materials

JF - Hanneng Cailiao/Chinese Journal of Energetic Materials

IS - 4

ER -

Energy characteristics computation of propellant containing octanitrocubane (ONC)

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