HYBRID ROCKET TURBINE ENGINE Russian patent published in 1998 - IPC

Abstract RU 2106511 C1

FIELD: manufacture of engines. SUBSTANCE: hybrid engine includes rocket turbine engine forming dual ramjet engine together with housing and movable casing. Mounted inside central body in shortened nozzle of external expansion is liquid-propellant rocket engine with annular combustion chamber and external expansion nozzle with central body inside which members of common turbopump unit are arranged. EFFECT: enhanced reliability. 1 dwg

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Authors

Porshnev V.A.

Fedorets N.V.

Dates

1998-03-10Published

1992-12-30Filed