The engine was a turbojet type with a single-spool 11-stage axial compressor, annular combustors, and 2-stage turbine. Turbine inlet temperature: 1,500 ☏ (816 ☌) The American manufacturing company Westinghouse had a contribution to the version by supplying an enhanced AN/APQ-36 aircraft fire control radar and J34-WE-36 turbojet engines.Oil system: pressure spray at 40 psi (275.8 kPa) dry sump, 60 S.U.Variants 19A Prototypes and initial production 19B Increased mass flow version delivering 1,400 lbf (6.23 kN) at 18,000 rpm at sea level J30-WE-20 production engines delivering 1,600 lbf (7.1 kN) thrust Applications
0 kommentar(er)
