A continuous combustion type engine. consists primarily of a compressor, nonaircraft gas turbine engine; chamber, combustion, nonaircraft gas turbine engine and a turbine assembly, nonaircraft gas turbine engine. it may have 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 and/or pneumatic 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 5950-00-295-8214
NSN 5950-01-479-8019
NSN 5985-00-050-0336
NSN 5895-00-187-5280
NSN 5999-00-925-9535
NSN 6320-00-731-6134
NSN 6685-01-019-7990
NSN 5910-01-381-3009
NSN 5915-01-303-0561
NSN 5990-01-633-9503
NSN 6110-00-232-5406
NSN 5945-01-420-8515