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 7035-00-206-6123
NSN 6610-00-088-9527
NSN 5920-01-510-9921
NSN 6620-01-245-0184
NSN 5960-01-483-9174
NSN 6685-01-492-6406
NSN 5915-01-326-1470
NSN 5910-01-364-8381
NSN 5998-00-848-9137
NSN 6220-01-098-8171
NSN 7035-00-238-3662
NSN 2925-00-978-8277