Accession Number : ADD009476
Title : Gas Turbine Cycle Providing a High Pressure Efflux.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON DC
Personal Author(s) : Reh,Frank J
Report Date : 14 May 1968
Pagination or Media Count : 3
Abstract : This invention relates to a system for developing propulsive thrust by the reaction of a flow of energized fluid and in particular is concerned with a gas turbine cycle of operation for developing the propulsive thrust.
Descriptors : *Patents, *Thrust, *Gas turbines, Propulsion systems, Compressors, High pressure compressors, Cycles, Inventions
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE