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Studying the Thermal Properties of a Cotton/Epoxy Composite Inhibitor
Author(s) -
Shahedifar Vahideh,
Tajik Hamid Reza,
Rezadoust Amir Masoud
Publication year - 2012
Publication title -
propellants, explosives, pyrotechnics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.56
H-Index - 65
eISSN - 1521-4087
pISSN - 0721-3115
DOI - 10.1002/prep.201100005
Subject(s) - thermogravimetric analysis , epoxy , composite number , differential scanning calorimetry , composite material , materials science , propellant , cellulose , ethyl cellulose , thermal analysis , chemical engineering , thermal , chemistry , polymer , organic chemistry , physics , meteorology , engineering , thermodynamics
The inhibitory effect of double‐base solid propellants is used to control and prevent the burning degree of exposed areas, induced by longer burning time. In recent years, inhibition with cellulose derivatives including cellulose acetate and ethyl cellulose has become popular, but these monolithic systems usually suffer from the drawback of a high erosion rate and demand high thickness and low burning time. A composite inhibitor based on cotton fibers/epoxy resin containing some chlorinated flame retardants (CFR), which were added in inhibitor composition to control its burning process, is described in this article. The thermal properties of the composite inhibitor were studied by thermogravimetric analysis (TGA), differential scanning calorimetry (DSC), thermomechanical analysis (TMA), and flame retardancy. Finally, the inhibited propellant charge, statically fired at ambient temperature, was found to display a smooth and flat pressure‐time profile, confirming the successful performance of the composite inhibition system without the application of any barrier coat.