associated with the compressor, burner, turbine and exhaust sections of the J34. These data are presented in the form of reproductions of oscillographic traces. However, because all of the air is passing through the whole. Disassembly & Reassembly of the Westinghouse J34 Turbojet Engine. of thrust, turned out to be the last production engine built by Westinghouse at its Aviation Gas Turbine Division facility in Kansas City, KS. Westinghouse J34 engine technologies, and built GE J-47 engines. Representative preliminary data showing the actual time response of these variables are presented. studies of turbine engine costs are Nelson (1977) and Birkler, Gar. Recordings of the response of the following parameters to step changes in power lever position throughout the available operating range of the engine were obtained ram pressure ratio, compressor-discharge pressure, exhaust-nozzle area, engine speed, turbine-outlet temperature, fuel-valve position, jet thrust, air flow, turbine-discharge pressure, fuel flow, throttle position, and boost-pump pressure. The object of the program was to determine the, steady-state stability and transient characteristics of the engine under control at various altitudes and ram pressure ratios, without afterburning. Preliminary Performance Data on Westinghouse Electronic Power Regulator Operating on J34-WE-32 Turbojet Engine in Altitude Wind Tunnel The behavior of the Westinghouse electronic power regulator operating on a J34-WE-32 turbojet engine was investigated in the NACA Lewis altitude wind tunnel at the request of the Bureau of Aeronautics, Department of the Navy.