2004
DOI: 10.2514/1.9234
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Chemical Kinetic Model for Monomethylhydrazine/Nitrogen Tetroxide Gas Phase Combustion and Hypergolic Ignition

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Cited by 67 publications
(43 citation statements)
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“…The current MMH/NTO hypergolic system has been used successfully for decades, 28,29 and much theoretical work on the MMH/NTO system has been performed. [30][31][32][33][34][35] However, little experimental work exists [36][37][38][39][40] to confirm these results. Therefore, replacing the volatile, highly toxic, and carcinogenic MMH with a safer fuel is not a straightforward task.…”
Section: Introductionmentioning
confidence: 99%
“…The current MMH/NTO hypergolic system has been used successfully for decades, 28,29 and much theoretical work on the MMH/NTO system has been performed. [30][31][32][33][34][35] However, little experimental work exists [36][37][38][39][40] to confirm these results. Therefore, replacing the volatile, highly toxic, and carcinogenic MMH with a safer fuel is not a straightforward task.…”
Section: Introductionmentioning
confidence: 99%
“…All of the theoretical studies suggested that the minimum activation energy of the H atom abstraction reactions for MMH + NO 2 would be larger than the activation energy of MMH + NO 2 → CH 3 NNH 2 + HONO included in the kinetics models proposed in the previous studies. 2,3 Moreover, the CH 3 NHNH + HONO formation path, which was the most energetically favorable path suggested by McQuaid and Ishikawa 5 and in our previous study, 7 was not taken into account in the current models.…”
Section: Introductionmentioning
confidence: 92%
“…For the efficient development of hypergolic propulsion systems, computational fluid dynamic models are employed to gain insight into the influence of design parameters on engine performance . The detailed chemical kinetic models, which are required for the accurate prediction of ignition phenomena, have been developed for hydrazine/NTO , MMH/NTO , and MMH/RFNA propellants.…”
Section: Introductionmentioning
confidence: 99%
“…For the efficient development of hypergolic propulsion systems, computational fluid dynamic models are employed to gain insight into the influence of design parameters on engine performance [1,2]. The detailed chemical kinetic models, which are required for the accurate prediction of ignition phenomena, have been developed for hydrazine/NTO [3], MMH/NTO [4], and MMH/RFNA [5] propellants. Although the abstraction of an H atom from CH 3 NHNH 2 by NO 2 plays an important role in the initiation of MMH/NTO or RFNA systems, the only CH 3 NNH 2 + HONO formation path with the activation energy of the rate coefficient estimated to be 25 kJ mol −1 , from the analogy of the NH 3 + NO 2 reaction, was involved in the above models [4,5].…”
Section: Introductionmentioning
confidence: 99%
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