TY - JOUR
T1 - Molecular revelation of the thermal decomposition mechanism of glycidyl azide polymer in nitrate esters matrix
AU - Fu, Jianbo
AU - Ren, Hui
AU - Liu, Xiaohan
AU - Sun, Jianjun
AU - Wu, Guoqing
N1 - Publisher Copyright:
© 2024
PY - 2024/10
Y1 - 2024/10
N2 - Glycidyl azide polymer (GAP), a high-energy and recyclable binder, can potentially enhance the energy of nitrate ester-plasticized polyether (NEPE) propellants. The thermal decomposition of binders in propellants is a crucial factor affecting engine safety. However, the thermal decomposition process of GAP in propellants remains unclear to date, and the precise atomic-level mechanism behind it remains elusive. In this study, we employed density functional theory (DFT) calculations and reactive force field molecular dynamics (ReaxFF-MD) simulations, combined with TG-DSC-FTIR-MS coupled tests, to investigate comprehensively the thermal decomposition process of GAP in nitrate esters matrix (NE-GAP). The study revealed that the decomposition process of NE-GAP involves five initial pathways and four stages. The nitrate esters (NEs) matrix provides a rich oxygen environment for GAP, resulting in a more complete decomposition process with minimal formation of clusters. In contrast to the pure component GAP (Pure-GAP), NE-GAP hardly generates amine products and uniquely forms C2O2 key intermediates. The decomposition products NO2 and NO of NEs preferentially attack the N1 on the azido groups and the H3 on the ether chains of GAP, constituting 43 % of the total initial reaction frequency. The presence of NEs reduces the activation energy (Ea) for azido group cleavage by 65 % and for ether bond cleavage by 66 %. These insights highlight potential pathways for preventing the thermal decomposition of GAP in NEPE propellants from an atomic and molecular perspective.
AB - Glycidyl azide polymer (GAP), a high-energy and recyclable binder, can potentially enhance the energy of nitrate ester-plasticized polyether (NEPE) propellants. The thermal decomposition of binders in propellants is a crucial factor affecting engine safety. However, the thermal decomposition process of GAP in propellants remains unclear to date, and the precise atomic-level mechanism behind it remains elusive. In this study, we employed density functional theory (DFT) calculations and reactive force field molecular dynamics (ReaxFF-MD) simulations, combined with TG-DSC-FTIR-MS coupled tests, to investigate comprehensively the thermal decomposition process of GAP in nitrate esters matrix (NE-GAP). The study revealed that the decomposition process of NE-GAP involves five initial pathways and four stages. The nitrate esters (NEs) matrix provides a rich oxygen environment for GAP, resulting in a more complete decomposition process with minimal formation of clusters. In contrast to the pure component GAP (Pure-GAP), NE-GAP hardly generates amine products and uniquely forms C2O2 key intermediates. The decomposition products NO2 and NO of NEs preferentially attack the N1 on the azido groups and the H3 on the ether chains of GAP, constituting 43 % of the total initial reaction frequency. The presence of NEs reduces the activation energy (Ea) for azido group cleavage by 65 % and for ether bond cleavage by 66 %. These insights highlight potential pathways for preventing the thermal decomposition of GAP in NEPE propellants from an atomic and molecular perspective.
KW - GAP
KW - Molecular simulation
KW - Nitrate Esters
KW - Thermal decomposition
UR - http://www.scopus.com/inward/record.url?scp=85200138468&partnerID=8YFLogxK
U2 - 10.1016/j.combustflame.2024.113648
DO - 10.1016/j.combustflame.2024.113648
M3 - Article
AN - SCOPUS:85200138468
SN - 0010-2180
VL - 268
JO - Combustion and Flame
JF - Combustion and Flame
M1 - 113648
ER -