LIQUID PROPELLANT ROCKET ENGINE INSTALLATION Russian patent published in 2002 - IPC

Abstract RU 2187010 C2

FIELD: rocketry. SUBSTANCE: liquid propellant rocket engine installation has torus-shaped propellant and oxidizer tanks with intake devices and engine arranged in free intra-torus space. Propellant and oxidizer tanks are made in form of segments of hollow torus limited at end faces by surfaces with nonzero curvature being the bottoms of tanks. EFFECT: reduced axial dimensions of liquid propellant rocket engine installation with resulting improved controllability of launch vehicle units furnished with proposed liquid propellant rocket engine installation. 1 dwg

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RU 2 187 010 C2

Authors

Ivanov M.Ju.

Katkov R.Eh.

Tupitsyn N.N.

Dates

2002-08-10—Published

2000-05-03—Filed