Compatibility of high energetic explosive TEX with components of propellants by DSC method

Rui Wang; Zi Hui Meng; Min Xue; Zhi Bin Xu; Ke Jian Cui; Feng Qi Zhao; Li Bai Xiao; Qi Guo

doi:10.14077/j.issn.1007-7812.2015.02.015

Compatibility of high energetic explosive TEX with components of propellants by DSC method

Rui Wang, Zi Hui Meng^*, Min Xue, Zhi Bin Xu, Ke Jian Cui, Feng Qi Zhao, Li Bai Xiao, Qi Guo

^*Corresponding author for this work

School of Chemistry and Chemical Engineering

Research output: Contribution to journal › Article › peer-review

8 Citations (Scopus)

Abstract

The thermal decomposition performance and compatibility of 4, 10-dinitro-2, 6, 8, 12-tatraoxa-4, 10-diazatatracyclo [5, 5, 0, 0^{5, 9}, 0^{3, 11}]-decane (TEX) with main components of propellants such as cyclotrimethylenetrinitramine(RDX), N-nitrodihydroxyethylaminedinitrate(DINA), nitrocellulose (NC), absorbentia(NC+NG), diethylphthalate(DEP), leadphthalate(Φ-Pb) and aluminium powder(micron order) were studied by differential scanning calorimetry(DSC). The results show that TEX is relatively stable to heat, the binary system of TEX was compatible with RDX, Φ-Pb, NC, DINA and aluminium powder, and was slightly sensitive with absorbentia(NC+NG) and NC. Thus TEX can be used as component in propellants.

Original language	English
Pages (from-to)	66-69
Number of pages	4
Journal	Huozhayao Xuebao/Chinese Journal of Explosives and Propellants
Volume	38
Issue number	2
DOIs	https://doi.org/10.14077/j.issn.1007-7812.2015.02.015
Publication status	Published - 1 Apr 2015

Keywords

4,10-dinitro-2,6,8,12-tatraoxa-4,10-diazatatracyclo[5,5,0,0, 0]-decane
Compatibility
Differential scanning calorimetry
Physical chemistry
Propellant
TEX

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10.14077/j.issn.1007-7812.2015.02.015

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@article{78f7ddf4754a4cc59023c33b1eb5afc6,

title = "Compatibility of high energetic explosive TEX with components of propellants by DSC method",

abstract = "The thermal decomposition performance and compatibility of 4, 10-dinitro-2, 6, 8, 12-tatraoxa-4, 10-diazatatracyclo [5, 5, 0, 05, 9, 03, 11]-decane (TEX) with main components of propellants such as cyclotrimethylenetrinitramine(RDX), N-nitrodihydroxyethylaminedinitrate(DINA), nitrocellulose (NC), absorbentia(NC+NG), diethylphthalate(DEP), leadphthalate(Φ-Pb) and aluminium powder(micron order) were studied by differential scanning calorimetry(DSC). The results show that TEX is relatively stable to heat, the binary system of TEX was compatible with RDX, Φ-Pb, NC, DINA and aluminium powder, and was slightly sensitive with absorbentia(NC+NG) and NC. Thus TEX can be used as component in propellants.",

keywords = "4,10-dinitro-2,6,8,12-tatraoxa-4,10-diazatatracyclo[5,5,0,0, 0]-decane, Compatibility, Differential scanning calorimetry, Physical chemistry, Propellant, TEX",

author = "Rui Wang and Meng, {Zi Hui} and Min Xue and Xu, {Zhi Bin} and Cui, {Ke Jian} and Zhao, {Feng Qi} and Xiao, {Li Bai} and Qi Guo",

year = "2015",

month = apr,

day = "1",

doi = "10.14077/j.issn.1007-7812.2015.02.015",

language = "English",

volume = "38",

pages = "66--69",

journal = "Huozhayao Xuebao/Chinese Journal of Explosives and Propellants",

issn = "1007-7812",

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T1 - Compatibility of high energetic explosive TEX with components of propellants by DSC method

AU - Wang, Rui

AU - Meng, Zi Hui

AU - Xue, Min

AU - Xu, Zhi Bin

AU - Cui, Ke Jian

AU - Zhao, Feng Qi

AU - Xiao, Li Bai

AU - Guo, Qi

PY - 2015/4/1

Y1 - 2015/4/1

N2 - The thermal decomposition performance and compatibility of 4, 10-dinitro-2, 6, 8, 12-tatraoxa-4, 10-diazatatracyclo [5, 5, 0, 05, 9, 03, 11]-decane (TEX) with main components of propellants such as cyclotrimethylenetrinitramine(RDX), N-nitrodihydroxyethylaminedinitrate(DINA), nitrocellulose (NC), absorbentia(NC+NG), diethylphthalate(DEP), leadphthalate(Φ-Pb) and aluminium powder(micron order) were studied by differential scanning calorimetry(DSC). The results show that TEX is relatively stable to heat, the binary system of TEX was compatible with RDX, Φ-Pb, NC, DINA and aluminium powder, and was slightly sensitive with absorbentia(NC+NG) and NC. Thus TEX can be used as component in propellants.

AB - The thermal decomposition performance and compatibility of 4, 10-dinitro-2, 6, 8, 12-tatraoxa-4, 10-diazatatracyclo [5, 5, 0, 05, 9, 03, 11]-decane (TEX) with main components of propellants such as cyclotrimethylenetrinitramine(RDX), N-nitrodihydroxyethylaminedinitrate(DINA), nitrocellulose (NC), absorbentia(NC+NG), diethylphthalate(DEP), leadphthalate(Φ-Pb) and aluminium powder(micron order) were studied by differential scanning calorimetry(DSC). The results show that TEX is relatively stable to heat, the binary system of TEX was compatible with RDX, Φ-Pb, NC, DINA and aluminium powder, and was slightly sensitive with absorbentia(NC+NG) and NC. Thus TEX can be used as component in propellants.

KW - 4,10-dinitro-2,6,8,12-tatraoxa-4,10-diazatatracyclo[5,5,0,0, 0]-decane

KW - Compatibility

KW - Differential scanning calorimetry

KW - Physical chemistry

KW - Propellant

KW - TEX

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SN - 1007-7812

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JO - Huozhayao Xuebao/Chinese Journal of Explosives and Propellants

JF - Huozhayao Xuebao/Chinese Journal of Explosives and Propellants

IS - 2

ER -

Compatibility of high energetic explosive TEX with components of propellants by DSC method

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