Was compressor rotor, axial, turbine engine
A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. it consists of disks, blades, hubs, and the like. it is the moving part of compressor, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5920-01-374-3802
NSN 5835-01-597-4820
NSN 5975-00-157-9676
NSN 6645-01-421-2445
NSN 5835-01-023-8733
NSN 6135-00-087-5300
NSN 6145-01-565-5595
NSN 5895-01-389-4015
NSN 6130-01-596-5774
NSN 5975-00-035-6524
NSN 6645-01-076-4655
NSN 6650-00-067-3572