Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
6594130 | Combustion and Flame | 2016 | 12 Pages |
Abstract
The burn rate of the propellant was evaluated and a lower pressure exponent is exhibited. This could be directly correlated to the thermal decomposition pattern of the cured binder and propellant. This study provides insight for processing energetic solid propellants wherein the basic decomposition mechanism of the new triazole-triazoline crosslinked polybutadiene based propellant binder and ballistics of the solid propellant processed using the new binder.
Keywords
Related Topics
Physical Sciences and Engineering
Chemical Engineering
Chemical Engineering (General)
Authors
S. Reshmi, K.P. Vijayalakshmi, Deepthi Thomas, R. Rajeev, C.P. Reghunadhan Nair,