Combustion characteristics and thermal behavior of modified double base propellant containing TNAD

Li Li; Qi Long Yan; Xiao Fei Qi; Hong Jian Yu

doi:10.3969/j.issn.1006-9941.2014.02.026

Combustion characteristics and thermal behavior of modified double base propellant containing TNAD

Li Li, Qi Long Yan, Xiao Fei Qi, Hong Jian Yu

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

Abstract

The combustion characteristics and thermal behavior of modified double base propellant containing Trans-1, 4, 5, 8-tetranitro-1, 4, 5, 8-tetraaza dacalin (TNAD) were investigated by burning rate test and PDSC. Results show that there was a general increase (greater than 9%) in burning rate when RDX is replaced by TNAD in propellant in the tested pressure range of 9-22 MPa. The pressure exponent in the pressure range of 9-15 MPa decreases from 0.26 to 0.18, but increases from 0.10 to 0.14 when the pressure is above 15 MPa. By analyzing from PDSC data, it is suggested that there is a strong interaction between NC/NG and TNAD, which increase the burning rate of propellant by enhancing the decomposition rate and heat release of the mixed system.

Original language	English
Pages (from-to)	256-258
Number of pages	3
Journal	Hanneng Cailiao/Chinese Journal of Energetic Materials
Volume	22
Issue number	2
DOIs	https://doi.org/10.3969/j.issn.1006-9941.2014.02.026
State	Published - Apr 2014
Externally published	Yes

Keywords

1, 4, 5, 8-tetranitro-1, 4, 5, 8-tetraazadecaline
Combustion characteristics
Modified double base propellant
Physical chemistry
Thermal behavior

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10.3969/j.issn.1006-9941.2014.02.026

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title = "Combustion characteristics and thermal behavior of modified double base propellant containing TNAD",

abstract = "The combustion characteristics and thermal behavior of modified double base propellant containing Trans-1, 4, 5, 8-tetranitro-1, 4, 5, 8-tetraaza dacalin (TNAD) were investigated by burning rate test and PDSC. Results show that there was a general increase (greater than 9%) in burning rate when RDX is replaced by TNAD in propellant in the tested pressure range of 9-22 MPa. The pressure exponent in the pressure range of 9-15 MPa decreases from 0.26 to 0.18, but increases from 0.10 to 0.14 when the pressure is above 15 MPa. By analyzing from PDSC data, it is suggested that there is a strong interaction between NC/NG and TNAD, which increase the burning rate of propellant by enhancing the decomposition rate and heat release of the mixed system.",

keywords = "1, 4, 5, 8-tetranitro-1, 4, 5, 8-tetraazadecaline, Combustion characteristics, Modified double base propellant, Physical chemistry, Thermal behavior",

author = "Li Li and Yan, {Qi Long} and Qi, {Xiao Fei} and Yu, {Hong Jian}",

year = "2014",

month = apr,

doi = "10.3969/j.issn.1006-9941.2014.02.026",

language = "英语",

volume = "22",

pages = "256--258",

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

issn = "1006-9941",

publisher = "Institute of Chemical Materials, China Academy of Engineering Physics",

number = "2",

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TY - JOUR

T1 - Combustion characteristics and thermal behavior of modified double base propellant containing TNAD

AU - Li, Li

AU - Yan, Qi Long

AU - Qi, Xiao Fei

AU - Yu, Hong Jian

PY - 2014/4

Y1 - 2014/4

N2 - The combustion characteristics and thermal behavior of modified double base propellant containing Trans-1, 4, 5, 8-tetranitro-1, 4, 5, 8-tetraaza dacalin (TNAD) were investigated by burning rate test and PDSC. Results show that there was a general increase (greater than 9%) in burning rate when RDX is replaced by TNAD in propellant in the tested pressure range of 9-22 MPa. The pressure exponent in the pressure range of 9-15 MPa decreases from 0.26 to 0.18, but increases from 0.10 to 0.14 when the pressure is above 15 MPa. By analyzing from PDSC data, it is suggested that there is a strong interaction between NC/NG and TNAD, which increase the burning rate of propellant by enhancing the decomposition rate and heat release of the mixed system.

AB - The combustion characteristics and thermal behavior of modified double base propellant containing Trans-1, 4, 5, 8-tetranitro-1, 4, 5, 8-tetraaza dacalin (TNAD) were investigated by burning rate test and PDSC. Results show that there was a general increase (greater than 9%) in burning rate when RDX is replaced by TNAD in propellant in the tested pressure range of 9-22 MPa. The pressure exponent in the pressure range of 9-15 MPa decreases from 0.26 to 0.18, but increases from 0.10 to 0.14 when the pressure is above 15 MPa. By analyzing from PDSC data, it is suggested that there is a strong interaction between NC/NG and TNAD, which increase the burning rate of propellant by enhancing the decomposition rate and heat release of the mixed system.

KW - 1, 4, 5, 8-tetranitro-1, 4, 5, 8-tetraazadecaline

KW - Combustion characteristics

KW - Modified double base propellant

KW - Physical chemistry

KW - Thermal behavior

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U2 - 10.3969/j.issn.1006-9941.2014.02.026

DO - 10.3969/j.issn.1006-9941.2014.02.026

M3 - 文章

AN - SCOPUS:84900470324

SN - 1006-9941

VL - 22

SP - 256

EP - 258

JO - Hanneng Cailiao/Chinese Journal of Energetic Materials

JF - Hanneng Cailiao/Chinese Journal of Energetic Materials

IS - 2

ER -

Combustion characteristics and thermal behavior of modified double base propellant containing TNAD

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Keywords

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