A continuous-combustion type engine, may be with or without container, designed to use superheated air to drive a turbine rotor which is connected to the rotorshaft of a helicopter by way of reduction gears.
Classification: Aircraft turbines (engines), except for use in civil aircraft, of a power not exceeding 5000 kw
NSN 5935-01-227-2829
NSN 6130-01-443-2448
NSN 5925-01-509-5267
NSN 5945-01-329-9479
NSN 5990-01-459-9533
NSN 5998-01-427-3776
NSN 5935-00-480-2054
NSN 5905-01-648-1888
NSN 5920-00-717-6839
NSN 5965-00-949-1599
NSN 5905-01-096-1758
NSN 2925-00-400-5634