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 5999-00-222-4808
NSN 5996-00-484-9196
NSN 5996-01-573-7953
NSN 5935-00-240-9500
NSN 5920-01-496-1309
NSN 5910-00-419-5330
NSN 5998-01-488-9859
NSN 7035-01-651-0678
NSN 6685-01-524-1997
NSN 5950-01-491-7501
NSN 6620-00-891-8584
NSN 6150-01-054-1696