TY - JOUR
T1 - Shock tube and laser absorption study of C–N–Cl interactions relevant to ammonium perchlorate combustion
AU - Song, Shubao
AU - Zhang, Lin
AU - Zou, Meishuai
AU - Shao, Jiankun
N1 - Publisher Copyright:
© 2025 The Combustion Institute
PY - 2025/12
Y1 - 2025/12
N2 - High-temperature gas-phase interactions between chlorine- and nitrogen-bearing species relevant to ammonium-perchlorate (AP) propellant combustion were elucidated by coupling shock-tube laser-absorption measurements with a detailed kinetic model. Time-resolved HCl concentration profiles were obtained for four argon-diluted surrogates—0.3 % NH3/0.3 % CCl4, 0.5 % NH3/0.3 % CCl4, 0.2 % NH3/0.2 % CCl4/0.2 % CH4, and 0.2 % NH3/0.2 % CCl4/0.2 % H2—over 1158–1506 K at near-atmospheric pressure. A kinetic model consisting of 164 species and 1358 reactions, assembled from state-of-the-art CCl4, H–Cl–O, NH3/C0–C2, and N–Cl sub-models, reproduced the new HCl data alongside literature ignition-delay and speciation measurements with excellent accuracy. Sensitivity and rate-of-production analyses reveal a temperature-robust control structure in which HCl forms almost entirely through Cl-atom abstraction from NH3, with Cl supplied by rapid CCl4 dissociation; the barrierless Cl + H<=>HCl path dominates in H2-containing mixtures, whereas competition from Cl + CH4<=>CH3 + HCl moderates HCl growth and channels carbon–nitrogen flux toward toxic HCN when CH4 is present. Elevated temperature chiefly amplifies Cl production and suppresses NH2 recombination, accelerating overall reactivity without altering the dominant pathways. The resulting benchmark HCl time-histories and rigorously validated model advance fundamental understanding of chlorine–nitrogen combustion chemistry and provide quantitative guidance for formulating halogenated energetic materials that maximise performance while limiting hazardous by-product formation. Importantly, the mechanism developed here may serve as a transferable gas-phase sub-model for future integration into comprehensive AP combustion frameworks, enabling more predictive simulations of real propellant systems.
AB - High-temperature gas-phase interactions between chlorine- and nitrogen-bearing species relevant to ammonium-perchlorate (AP) propellant combustion were elucidated by coupling shock-tube laser-absorption measurements with a detailed kinetic model. Time-resolved HCl concentration profiles were obtained for four argon-diluted surrogates—0.3 % NH3/0.3 % CCl4, 0.5 % NH3/0.3 % CCl4, 0.2 % NH3/0.2 % CCl4/0.2 % CH4, and 0.2 % NH3/0.2 % CCl4/0.2 % H2—over 1158–1506 K at near-atmospheric pressure. A kinetic model consisting of 164 species and 1358 reactions, assembled from state-of-the-art CCl4, H–Cl–O, NH3/C0–C2, and N–Cl sub-models, reproduced the new HCl data alongside literature ignition-delay and speciation measurements with excellent accuracy. Sensitivity and rate-of-production analyses reveal a temperature-robust control structure in which HCl forms almost entirely through Cl-atom abstraction from NH3, with Cl supplied by rapid CCl4 dissociation; the barrierless Cl + H<=>HCl path dominates in H2-containing mixtures, whereas competition from Cl + CH4<=>CH3 + HCl moderates HCl growth and channels carbon–nitrogen flux toward toxic HCN when CH4 is present. Elevated temperature chiefly amplifies Cl production and suppresses NH2 recombination, accelerating overall reactivity without altering the dominant pathways. The resulting benchmark HCl time-histories and rigorously validated model advance fundamental understanding of chlorine–nitrogen combustion chemistry and provide quantitative guidance for formulating halogenated energetic materials that maximise performance while limiting hazardous by-product formation. Importantly, the mechanism developed here may serve as a transferable gas-phase sub-model for future integration into comprehensive AP combustion frameworks, enabling more predictive simulations of real propellant systems.
KW - Ammonium perchlorate
KW - Kinetic model
KW - Laser absorption spectroscopy
KW - Pyrolysis
KW - Shock tube
UR - https://www.scopus.com/pages/publications/105017238119
U2 - 10.1016/j.combustflame.2025.114508
DO - 10.1016/j.combustflame.2025.114508
M3 - Article
AN - SCOPUS:105017238119
SN - 0010-2180
VL - 282
JO - Combustion and Flame
JF - Combustion and Flame
M1 - 114508
ER -