KINETICS OF THERMAL GAS-PHASE DECOMPOSITION OF 2-BROMOPROPENE USING STATIC SYSTEM
5
Table IV Comparison of Arrhenius Parameters Determined by Various Methods for Thermal Decomposition of
2-Bromopropene
Method
Temperature (K)
E (kJ mol−1
)
log A (s−1
)
r
Reference
a
Shock tube (at 100 Torr)
Static system
RRKM
1078.4–1221
570.9–654.2
720–840
274.4
208.2
203.8
14.93
13.47
13.03
0.9977
0.9952
1
[7]
This work
This work
r = Correlation coefficient.
reactions. Tsang, while comparing the experimental
results with the calculated results for decomposition
pressure, can be represented by
0.6
6.7(kJ mol−1)/RT
k(total) = 1013.47
exp−208.2
of 3-C3H5Br, observed that a satisfactory A factor is
∝
not obtained unless the moment of inertia of the two-
dimensional rotor is lowered from 9 × 10−39 g cm2 to
0.54 × 10−39 g cm2 [14]. For this, he followed the Ben-
son’s prescription of a “hindered rotor” transition state
[15].
The pressure dependence study and RRKM calcu-
lation indicate that the Arrhenius parameters obtained
in this work are the high pressure limiting values.
The RRKM-treated data exactly reproduce the
experimental rate constants over the entire tempera-
ture and pressure range studied.
An exact fit can be made when we use a slightly
lower value of β (collision efficiency) 0.2–0.6. In
the present investigations, we use β = 0.4. The same
conclusion has also been drawn by Tsang in his report
on 3-C3H5Br decomposition.
BIBLIOGRAPHY
A combined Arrhenius plot of the present static,
shock tube (at 100 Torr) and RRKM-treated data (in
the temperature range of 720–840 K) is represented
in Fig. 6, showing a good agreement between static
and RRKM-treated data, but no satisfactory agreement
of shock tube investigations with static and RRKM-
treated data is observed. A comparison of Arrhenius
parameters determined by all the three methods is given
in Table IV. It can be seen from the table that the
Arrhenius parameters deduced from the static system
and RRKM-treated data are in consonant with each
other but deviate considerably from the shock tube
determinations.
1. Maccoll, A. Adv Phys Org Chem 1965, 91, 3.
2. Maccoll, A. Chem Rev 1969, 69, 33.
3. Benson, S. W.; O’Neal, H. E. Kinetic Data on Gas Phase
Unimolecular Reactions, NSRDS-NBS 21, 1970.
4. Manion, J. A.; Louw, R. J Chem Soc, Perkin Trans 1988,
2, 1547.
5. Zabel, F. Int J Chem Kinet 1977, 9, 6551.
6. Shilov, A. E.; Sbirova, R. D. Kinet Catal 1964, 5, 32.
7. Roy, K.; Awan, I. A.; Manion, J. A.; Tsang, W. Phys
Chem Chem Phys 2003, 5, 1806.
8. Awan, I. A.; Mahmood, T. J Chem Soc Pak 1999, 21(2),
87.
9. Laws, P. A.; Hayley, B. D.; Anthony, L. M.; Roscoe,
J. M. J Phys Chem A 2001, 105, 1830.
10. Thomas, P. J. J Chem Soc 1959, 1192.
11. Maccoll, A.; Thomas, P. J. Chem Soc 1955, 969.
12. Lee, M.; Kim, M. S. J Chem Phys 2003, 119(23), 12351.
13. NIST Chemistry Webbook, NIST Standard Reference
Data, no. 69, National Institute of Standards and Tech-
nology: Gaithersburg, MD, 2005.
14. Tsang, W. J Phys Chem 1984, 88, 2812.
15. Benson, S. W. Thermochemical Kinetics; Wiley:
New York, 1976.
CONCLUSION
2-Bromopropene decomposes in the temperature range
570.9–654.2 K to give propyne and hydrogen bromide.
The decomposition proceeds by a unimolecular mech-
anism. The decomposition obeys first-order kinetics,
and the rate constant, which is independent of initial
International Journal of Chemical Kinetics DOI 10.1002/kin