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 6650-01-462-5879
NSN 5945-01-095-9020
NSN 5950-01-383-8341
NSN 6650-01-100-0933
NSN 5895-00-539-8322
NSN 5975-01-551-1720
NSN 6620-01-065-8265
NSN 6110-01-167-6009
NSN 5950-00-179-0189
NSN 2925-00-120-9302
NSN 2925-00-028-1481
NSN 7035-01-633-9537