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 5930-01-564-9916
NSN 6645-00-920-8690
NSN 5975-00-698-9853
NSN 5925-00-803-5491
NSN 6620-01-363-0499
NSN 5965-00-350-2367
NSN 6135-01-222-0703
NSN 6150-00-265-7799
NSN 6130-01-025-3378
NSN 5855-01-544-1482
NSN 5935-00-567-8301
NSN 6620-00-266-2763