Improving the Mechanical Properties of Glycidyl Azide Polymeric Matrix Used in Composite Solid Rocket Propellant by Adding Advanced Cross-Linker
Author:
Affiliation:
1. Beijing University of Aeronautics and Astronautics; Beijing P. R. China
2. Military Technical College; Kobry Elkobbah Cairo Egypt
Publisher
Wiley
Subject
Inorganic Chemistry
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/zaac.201900003/fullpdf
Reference33 articles.
1. Arab. J. Chem 2014
2. Development of Modern Solid Propellants
3. Application of vacuum stability test to determine thermal decomposition kinetics of nitramines bonded by polyurethane matrix
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