FIELD: chemistry.
SUBSTANCE: invention relates to propellants for liquid, solid fuel and hybrid rocket engines, containing oxidiser and combustibles. Propellant oxidiser contains boron nitrate. Propellant contains saod oxidiser and combustibles, such as pure or bound boron, for instance boranes (diborane), beryllium borohydrate, boron carbide, borides of metals. In addition to large release of hydrogen born reacts with released nitrogen with formation of boron nitride and heat release 252.6 kJ/mol.
EFFECT: obtaining propellant oxidiser, which contains boron nitrate.
4 cl
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