Abstract

Effect of some bis(ethylenediamine)metal nitrate (BEMN) complexes, i.e. [M(en) 2 [(NO 3 ) 2 (where, M = Cu, Co, Ni and Zn and en = ethylenediamine) during the condensed phase thermolysis of hydroxyl-terminated polybutadiene(HTPB) and ammonium perchlorate (AP) composite solid propellants (CSPs) has been studied using TG and DTA. The results indicate that the thermolysis of propellants is affected when these energetic complexes are used as burning rate modifiers in small percentage (2% by wt). Ignition delay (t i d ) measurements on unmodified and modified propellants have been conducted to examine the effect of these additives during the rapid thermolysis of propellants. The response of the modified propellants to drop weight impact is determined to know the safety aspects. The effect of these additives on thermal decomposition of oxidizer (AP) is also investigated. Copper and cobalt complexes show considerable effect while nickel and zinc moderate effect on both propellants and AP decomposition.

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.