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 5915-00-548-1434
NSN 5975-00-283-1320
NSN 5905-01-054-3805
NSN 5835-01-270-7899
NSN 6240-01-428-9410
NSN 5950-01-424-3233
NSN 5965-00-729-6835
NSN 6150-00-905-8277
NSN 2925-01-532-8445
NSN 6105-01-537-9207
NSN 6320-01-183-8196
NSN 6110-00-134-1534