TRIAZOLE CROSSLINKED HIGH BURN RATE DEFECT FREE SOLID PROPELLANTS BASED ON POLYMERIC AZIDE BINDER

摘要

The present application relates to the field of propellant technology and discloses composite solid propellant compositions which are based on an azide polymer crosslinked through triazoles as binder, and a process for their preparation. The propellant compositions provided herein are defect free, void free and have a high burn rate.