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 6110-00-453-5839
NSN 5950-00-018-8235
NSN 6220-01-363-4772
NSN 6645-01-376-2336
NSN 5930-01-253-0642
NSN 5960-01-512-0233
NSN 6105-00-316-5098
NSN 5915-01-025-0346
NSN 5920-01-607-0771
NSN 6105-01-082-2923
NSN 5905-01-291-8011
NSN 5855-01-264-8599