Synthesis and properties of energetics metal borides for hybrid solid-propellant rocket engines S. S. Bondarchuk, A. E. Matveev, V. V. Promakhov [et al.]
Material type:
ArticleSubject(s): бориды металлов | высокоэнергетические материалы | твердотопливные ракетные двигателиGenre/Form: статьи в сборниках Online resources: Click here to access online
In:
Proceedings of the Scientific-practical conference "Research and development - 2016", 14-15 December 2016, Moscow, Russia P. 511-518Abstract: In this paper, the problems of production and characterization of
microsized metal borides (including aluminum, titanium, magnesium) are
discussed. The preferences of application for high-energy materials are presented.
The problems of chemical stability and chemical compatibility are discussed.
A technique for production of metal borides is also described which is known as
self-propagating high-temperature synthesis (SHS) and the subsequent mechanical
treatment. The result is microsized borides which have an average size of around 5
microns with a sharp curve for distribution sizes. The purity is enough for use as
fuel of high-energy materials hybrid solid-propellant rocket engines. The results of
SEM, X-Ray, DSC, and TG analyses are also presented and discussed.
Библиогр.: 8 назв.
In this paper, the problems of production and characterization of
microsized metal borides (including aluminum, titanium, magnesium) are
discussed. The preferences of application for high-energy materials are presented.
The problems of chemical stability and chemical compatibility are discussed.
A technique for production of metal borides is also described which is known as
self-propagating high-temperature synthesis (SHS) and the subsequent mechanical
treatment. The result is microsized borides which have an average size of around 5
microns with a sharp curve for distribution sizes. The purity is enough for use as
fuel of high-energy materials hybrid solid-propellant rocket engines. The results of
SEM, X-Ray, DSC, and TG analyses are also presented and discussed.
There are no comments on this title.