CH + NO -> H + NCO
k = 2.00E+13 cm3/mol s
SOURCE:
From data of
- Dean, A.J., Hanson, R.K., and Bowman, C.T.
(1991) J. Phys. Chem. 95, 3180;
- Becker, K.H., Engelhardt, B., Geiger, H., Kurtenbach, R., and
Wiesen, P. (1993) Chem. Phys. Letters 210, 135.
- Lambrecht, R.K., and Hershberger, J.F.
(1994) J. Phys. Chem. 98, 8406.
- Markus, M.W., and Roth, P. (1995)
Shock Waves @ Marseille II, Springer-Verlag
(Brun, R., and Drunitrescu, L.Z. eds.) p. 95.
- as analyzed by
Dean, A.M., and Bozzelli, J.W. (1996)
in Combustion Chemistry II, Springer-Verlag, New York.
- COMMENTS:
-
Served as an optimization variable in GRI-Mech 2.1 release.
The rate coefficient value was not changed.
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Temp delta-S delta-H kf kr Keq
(K) (cal/mol K) (kcal/mol) ----(mol,cm3,s)-----
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300 -11.2 -81.0 2.00E+13 5.61E-44 3.56E+56
500 -10.5 -80.7 2.00E+13 2.09E-20 9.55E+32
1000 -8.9 -79.5 2.00E+13 7.36E-03 2.72E+15
1500 -8.0 -78.4 2.00E+13 4.21E+03 4.75E+09
2000 -7.5 -77.6 2.00E+13 2.93E+06 6.84E+06
2500 -7.2 -77.0 2.00E+13 1.43E+08 1.40E+05
3000 -7.1 -76.5 2.00E+13 1.88E+09 1.07E+04
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