PROPELLANT FOR LIQUID PROPELLANT ROCKET ENGINES Russian patent published in 2004 - IPC

Abstract RU 2233385 C2

FIELD: rocketry.

SUBSTANCE: proposed propellant for liquid propellant rocket engine contains hydrocarbon fuel. Used as such fuel is I-methyl 1.2 dicyclopropyl-cyclopropane. Invention makes it possible to get higher density of rocket propellant as compared with propellants on kerosene and dicyclobutyl base.

EFFECT: provision of higher increment of specific impulse.

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RU 2 233 385 C2

Authors

Semenov Ju.P.

Sokolov B.A.

Chernykh S.P.

Grigor'Ev Anatolij Aleksandrovich

Nefedov O.M.

Istomin N.N.

Shirshov G.M.

Dates

2004-07-27Published

2002-10-01Filed