Combustion and thermal decomposition of HNIW and HTPB/HNIW propellants with additives

Rongjie Yang; Hongmei An; Huimin Tan

doi:10.1016/j.combustflame.2003.08.008

Combustion and thermal decomposition of HNIW and HTPB/HNIW propellants with additives

Rongjie Yang^*, Hongmei An, Huimin 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

50 引用（Scopus）

摘要

The relation between burning rate and pressure was obtained for the monopropellant HNIW with some metal oxides and organometallic salts added. It was found that PbO, Fe₂O₃, CuO, etc. did not decrease the exponent for the dependence of burning rate on pressure; but some organometallic salts did. The combustion characteristics of HTPB/HNIW composite solid propellants were also studied. Photographs of the flame structure of HNIW propellants were taken. The thermal decomposition of these propellants with organometallic salts added were studied using DSC and in situ FTIR. Some additives inhibit the thermal decomposition of HNIW.

源语言	英语
页（从-至）	463-473
页数	11
期刊	Combustion and Flame
卷	135
期	4
DOI	https://doi.org/10.1016/j.combustflame.2003.08.008
出版状态	已出版 - 12月 2003

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title = "Combustion and thermal decomposition of HNIW and HTPB/HNIW propellants with additives",

abstract = "The relation between burning rate and pressure was obtained for the monopropellant HNIW with some metal oxides and organometallic salts added. It was found that PbO, Fe2O3, CuO, etc. did not decrease the exponent for the dependence of burning rate on pressure; but some organometallic salts did. The combustion characteristics of HTPB/HNIW composite solid propellants were also studied. Photographs of the flame structure of HNIW propellants were taken. The thermal decomposition of these propellants with organometallic salts added were studied using DSC and in situ FTIR. Some additives inhibit the thermal decomposition of HNIW.",

keywords = "CL-20, Combustion, HNIW, Hexanitrohexaazaisowurtzitane, Hydroxyl-terminated polybutadiene, Solid propellant",

author = "Rongjie Yang and Hongmei An and Huimin Tan",

year = "2003",

month = dec,

doi = "10.1016/j.combustflame.2003.08.008",

language = "English",

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journal = "Combustion and Flame",

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TY - JOUR

T1 - Combustion and thermal decomposition of HNIW and HTPB/HNIW propellants with additives

AU - Yang, Rongjie

AU - An, Hongmei

AU - Tan, Huimin

PY - 2003/12

Y1 - 2003/12

N2 - The relation between burning rate and pressure was obtained for the monopropellant HNIW with some metal oxides and organometallic salts added. It was found that PbO, Fe2O3, CuO, etc. did not decrease the exponent for the dependence of burning rate on pressure; but some organometallic salts did. The combustion characteristics of HTPB/HNIW composite solid propellants were also studied. Photographs of the flame structure of HNIW propellants were taken. The thermal decomposition of these propellants with organometallic salts added were studied using DSC and in situ FTIR. Some additives inhibit the thermal decomposition of HNIW.

AB - The relation between burning rate and pressure was obtained for the monopropellant HNIW with some metal oxides and organometallic salts added. It was found that PbO, Fe2O3, CuO, etc. did not decrease the exponent for the dependence of burning rate on pressure; but some organometallic salts did. The combustion characteristics of HTPB/HNIW composite solid propellants were also studied. Photographs of the flame structure of HNIW propellants were taken. The thermal decomposition of these propellants with organometallic salts added were studied using DSC and in situ FTIR. Some additives inhibit the thermal decomposition of HNIW.

KW - CL-20

KW - Combustion

KW - HNIW

KW - Hexanitrohexaazaisowurtzitane

KW - Hydroxyl-terminated polybutadiene

KW - Solid propellant

UR - http://www.scopus.com/inward/record.url?scp=0347511630&partnerID=8YFLogxK

U2 - 10.1016/j.combustflame.2003.08.008

DO - 10.1016/j.combustflame.2003.08.008

M3 - Article

AN - SCOPUS:0347511630

SN - 0010-2180

VL - 135

SP - 463

EP - 473

JO - Combustion and Flame

JF - Combustion and Flame

IS - 4

ER -

Combustion and thermal decomposition of HNIW and HTPB/HNIW propellants with additives

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