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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Authors
Dates
2004-07-27—Published
2002-10-01—Filed