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 5935-00-119-9061
NSN 5925-01-303-8381
NSN 5950-01-285-2449
NSN 2925-00-149-0760
NSN 6145-01-109-6126
NSN 4140-01-525-7692
NSN 6320-01-449-1014
NSN 7035-01-049-6776
NSN 5905-01-432-1961
NSN 6320-01-207-0636
NSN 6685-00-270-8070
NSN 6150-00-518-1402