ROCKET ENGINE Russian patent published in 1994 - IPC

Abstract RU 2009354 C1

FIELD: engines. SUBSTANCE: turbine 5 of a thermoemission electric current generator is used as a power source. Conductor 9 of the generator is mounted on dielectric posts 10 around a chamber in the area of the critical section of the nozzle. Cathodes 11 are made in the form of heat tubes which one end is passed into the engine nozzle, and the other one - into the conductor cavity and is covered by an alkaline metal layer. EFFECT: improved efficiency. 1 dwg

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RU 2 009 354 C1

Authors

Spirjakov Gennadij Nikolaevich

Dates

1994-03-15—Published

1991-06-20—Filed