Preliminary research of composite rocket propellants with hexogen and titanium oxide powder

Composite solid propellants based on ammonium perchlorate/hydroxyl-terminated polybutadiene/isophorone dyisocyanate including two levels of hexogen (RDX) are presented in this paper. The mass of RDX increased in relation to oxidant, with constant bimodal fraction ratio. Combustion of the propellants...

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Bibliographic Details

Published in:	Scientific Technical Review
Main Authors:	Rodić Vesna, Bogosavljević Marica, Milojković Aleksandar, Mijatov Slavko
Format:	Article
Language:	English
Published:	Military Technical Institute, Belgrade 2018-01-01
Subjects:	composite solid propellant ammonium perchlorate hydroxyl-terminated polybutadiene hexogen titanium (iv)oxide ballistic characteristics thermochemical parameters
Online Access:	https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2018/1820-02061802036R.pdf