FIELD: aviation.
SUBSTANCE: hypergolic propellant, self-igniting in contact with an oxidizer, consists of fuel with pyrotechnic additive and oxidizer in which water solutions of hydrogen peroxide with concentration of 81.5-98 wt % are used as an oxidizer, and kerosene with dissolved in it pyrophoric high-active additive, the content of which is 10-15% by weight of the fuel weight, is used as fuel. The additive is a mixture comprising 87% by weight of triethyl boron and 13% by weight of triethylaluminum.
EFFECT: use of propellant makes it possible to improve the stability of combustion of components, to facilitate the start-up and simplify the construction of liquid rocket engine because of lack of ignition system.
3 dwg, 1 tbl, 2 ex
