Kinetic parameters of composite propellants from thermogravimetric data
Journal Article
·
· Combustion and Flame
- Royal Military College of Canada, Kingston, Ontario (Canada). Dept. of Mechanical Engineering
- Defence Research Establishment, Courcelette, Quebec (Canada)
This paper presents a method of estimating all three global kinetic parameters, A (preexponential factor), E (energy of activation), and n (reaction order), from the results of a single dynamic (nonisothermal) thermogravimetry (TG) run on a propellant sample. The procedure will also show how satisfactorily pyrolysis of the propellant can be represented by the simple relation of Eq. 4 (d{alpha}/dT = (1{minus}{alpha}){sup n}(A/{phi})e{sup {minus}E/RT}) with constant values of A, E, and n where {alpha} = fractional reaction, T = temperature, {phi} = programmed increase in T, and R = universal gas constant.
- OSTI ID:
- 89640
- Journal Information:
- Combustion and Flame, Vol. 102, Issue 1-2; Other Information: PBD: Jul 1995
- Country of Publication:
- United States
- Language:
- English
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