Rotor diameter is 13.692min to 13.696 max high
A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, nonaircraft gas turbine engine and/or the rotor, fan, nonaircraft gas turbine engine through a shaft, turbine, nonaircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, nonaircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, nonaircraft gas turbine engine.
Classification: Parts of nonaircraft gas turbines
NSN 6610-01-273-2075
NSN 5895-01-085-5471
NSN 5996-01-281-9840
NSN 5910-00-399-7455
NSN 5975-00-446-7875
NSN 6105-01-061-1242
NSN 6320-00-925-0558
NSN 5855-01-133-3587
NSN 5950-00-372-5591
NSN 6240-01-195-8696
NSN 5990-01-378-7349
NSN 6650-00-170-5095