Preliminary research of composite rocket propellants including octogene

Preliminary research of composite rocket propellants including octogene

Composite solid propellants based on ammonium perchlorate/hydroxyterminated polybutadiene/isophorone dyisocyanate including different contents of octogene (HMX) have been represented in this paper. The mass of HMX increased in relation to oxidant, with constant bimodal fraction ratio. Combustion of...

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Bibliographic Details
Main Authors: Rodić Vesna, Bogosavljević Marica, Milojković Aleksandar, Brzić Saša, Fidanovski Bojana, Gligorijević Nikola
Format: Article
Language:English
Published: Military Technical Institute, Belgrade 2017-01-01
Series:Scientific Technical Review
Subjects:
composite rocket propellant
ammonium perchlorate
hydroxyterminated polybutadien
octogen
titanium (iv) oxide
ballistic properties
burning rate
mechanical characteristics
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2017/1820-02061701003R.pdf

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