KHD T117 Turbojet Engine

 

 

KHD T117 Specification

Power Output........................................ RPM..................................................... Compressor........................................... Combustion Chamber............................ Turbine.................................................. Layout................................................... Starting................................................. Ignition.................................................. Fuel System............................... .......... Lubrication............................................ Oil Spec................................................ Accessories........................................... Weight.................................................. Application...........................................

Up to 236 Lbs thrust 45,000 estimated maximum Centrifugal Impeller PR 5.5:1 Mass Flow 1.6kg/sec Reverse Flow Annular with 12 vapourising burners 1 Stage Axial Flow Single Spool with Accessory Gearbox in Nose Air Impingement Tourch Ignitor with HT Plug Engine Driven Gear Pump , Electronic Control. Return System, Engine Driven Gear Pump, Integral Tank Aeroshell 390, MIL-L-7808 Alternator mounted in nose 23kg Target Drone/RPV