Kinetic parameters of composite propellants from thermogravimetric data
β Scribed by V.K. Rao; M.F. Bardon; R.A. Stowe
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 403 KB
- Volume
- 102
- Category
- Article
- ISSN
- 0010-2180
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β¦ Synopsis
T* preexponential factor energy of activation sample mass initial sample mass final sample mass reaction order universal gas constant time time-to-ignition temperature temperature at which reaction commences surface temperature of hot plate initial temperature temperature at which reaction rate is maximum Greek Symbols ff cY* fractional reaction fractional reaction at T* maximum reaction rate with respect to temperature COMBUSTIONAND FLAME 102: 219-225 (1995)
π SIMILAR VOLUMES
In a recent communication by Rao et al. [ll, the authors presented a method for calculating the kinetic parameters for the hetrogeneous ieaction of rocket propellents. In order to complete their solution, they needed to evaluate the integral of the Boltzman Factor given by h(T) = /Te-E/RTdT. 0 They