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 5975-01-411-7471
NSN 6130-01-429-9319
NSN 5930-01-390-7730
NSN 5996-00-253-7148
NSN 5910-01-485-5051
NSN 7035-00-238-3662
NSN 6645-01-175-1392
NSN 5915-01-010-1562
NSN 5990-00-295-7068
NSN 6685-01-422-3514
NSN 5925-00-566-4169
NSN 5999-00-766-7472