A continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft, pneumatic power or thrust power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.
Classification: Gas turbine engine, except aircraft nesoi, of a power not exceeding 5,000 kw
NSN 2925-00-928-5931
NSN 7035-01-394-1324
NSN 5910-00-343-9585
NSN 6620-00-185-1614
NSN 5945-01-516-2931
NSN 6240-00-144-4693
NSN 6145-00-433-8735
NSN 5835-01-392-7683
NSN 6240-01-321-7844
NSN 5999-01-445-6972
NSN 2925-01-577-0004
NSN 4140-01-531-3080