2018
DOI: 10.1016/j.combustflame.2018.10.005
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Improvement and validation of a detailed reaction mechanism for thermal decomposition of RDX in liquid phase

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Cited by 24 publications
(12 citation statements)
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“…In the later stage, the production of N2 and CO2 are observed, and the overall reactions reach an equilibrium after 100 ps. The production of NO2, NO, HNO2, H2O, and CO2 is also reported in a recent FTIR experiment 40 .The RDX decomposes into NO2, NO and H2O first, and then NO2 and NO starts to decrease after a certain time, while H2O continues to increase. Although the experiments 40 are performed at a lower temperature (e.g.…”
Section: Species Evolution During Rdx Decompositionsupporting
confidence: 71%
“…In the later stage, the production of N2 and CO2 are observed, and the overall reactions reach an equilibrium after 100 ps. The production of NO2, NO, HNO2, H2O, and CO2 is also reported in a recent FTIR experiment 40 .The RDX decomposes into NO2, NO and H2O first, and then NO2 and NO starts to decrease after a certain time, while H2O continues to increase. Although the experiments 40 are performed at a lower temperature (e.g.…”
Section: Species Evolution During Rdx Decompositionsupporting
confidence: 71%
“…Using the couple cluster theory, the E a value of the HONO elimination has been calculated to be lower than that of the N-NO 2 homolytic reaction for RDX [63]. A recent study of the initial decomposition process of liquid RDX has revealed that HONO elimination is likely to be the major decomposition pathway [64].…”
Section: Nitraminesmentioning
confidence: 99%
“…However, careful analyses of cook-off experiments have shown that multistep reaction schemes are required to model those response characteristics [5][6][7]. The modelling of propellant combustion processes (especially those containing high explosive constituents HMX and RDX) are quite generally written as containing multiple steps, which are necessary to describe the observed flame structure and its dependence on the confining pressure [8][9][10][11]. Defining the deflagration rates of such materials under moderately high pressures requires an understanding of this staged reaction process (preferably expressed in an Arrhenius form) and how temperature and pressure evolve in the flame structure [12].…”
Section: Introductionmentioning
confidence: 99%
“…However, despite this long-standing interest, there is little that is directly known about these reaction processes in the condensed phase. While the later time (and lower pressure) reactions in propellant combustion flame structures can be well-studied, the initial processes in the condensed phase are more conjectural [8][9][10][11]. The direct observation of reaction processes in solid materials, particularly under shock-loading, has proven to be quite difficult, being frustrated by optical constraints and the rapid reaction rates at appropriate conditions [18][19][20].…”
Section: Introductionmentioning
confidence: 99%
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