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 5996-01-646-1264
NSN 5985-00-671-9707
NSN 5935-00-807-9308
NSN 6105-01-394-5721
NSN 6685-00-784-0516
NSN 5960-01-157-7009
NSN 5985-01-081-4498
NSN 5999-01-344-8741
NSN 6610-01-522-5751
NSN 5930-01-273-0946
NSN 6105-00-194-8814
NSN 6135-01-327-2092