ROCKET PROPELLANT OR EXPLOSIVE SUBSTANCE AND METHOD OF ITS PREPARATION (VERSIONS) Russian patent published in 2014 - IPC C06B25/00 C06D5/00 

FIELD: chemistry.

SUBSTANCE: invention relates to versions of rocket fuel for solid-propellant and hybrid rocket engines. Rocket propellant contains nitro-compound, for instance, nitroform, which is present in it in bound connection with unsaturated hydrocarbons (nitroethylene, ethylene, sterene, propylene, nitropropylene, acrylic acid nitryl, diacetylene) by Michael reaction. As oxidizer propellant contains, for instance ammonium dinitramide. In another version nitroform in rocket propellant is dissolved in liquid ammonia. Rocket propellant can contain boron compound, for instance, decaborane, diborane, pentaborane.

EFFECT: improvement of rocket propellant for solid-propellant and hybrid rocket engines.

8 cl