FIELD: chemistry.
SUBSTANCE: propellant contains fuel and oxidiser. As fuel it contains lithium-aluminium borohydrate, lithium-aluminium hydrate, silicon borohydrate, silane, diborane, tetraborane, decaborane, beryllium borohydrate, as oxidiser - ammonium dinitramide, ammonium nitrate, nitric acid and has such component ratio that engine releases only pure hydrogen as gases. Fuel con include additional quantity of borane, for instance, tetraborane, and retarding additive -orthoboric acid.
EFFECT: increased rate of jet stream and specific impulse of rocket engine, even without extending nozzle.
14 cl
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Authors
Dates
2015-12-10—Published
2014-05-13—Filed