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.
NSN 5920-01-122-0477
NSN 6240-01-349-8766
NSN 2925-01-443-5929
NSN 6240-01-273-4903
NSN 5945-01-407-5571
NSN 5855-01-295-2313
NSN 5950-00-855-0469
NSN 5975-01-046-5166
NSN 6105-01-071-1367
NSN 5915-01-599-4159
NSN 5960-01-560-8461
NSN 5930-01-119-2732