Kinetic parameters of composite propellants from thermogravimetric data

Journal Article · Sat Jul 01 04:00:00 EDT 1995 · Combustion and Flame

DOI:https://doi.org/10.1016/0010-2180(95)00078-K· OSTI ID:89640

Rao, V K; Bardon, M F ^[1]; Stowe, R A ^[2]

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1. Royal Military College of Canada, Kingston, Ontario (Canada). Dept. of Mechanical Engineering
2. 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, Journal Name: Combustion and Flame Journal Issue: 1-2 Vol. 102; ISSN CBFMAO; ISSN 0010-2180
• Country of Publication: United States
• Language: English

Related Subjects

40 CHEMISTRY
ACTIVATION ENERGY
AMMONIUM NITRATES
COMBUSTION KINETICS
EXPERIMENTAL DATA
PROPELLANTS
PYROLYSIS
THERMAL GRAVIMETRIC ANALYSIS
THERMODYNAMIC PROPERTIES