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 5990-01-246-2488
NSN 6685-01-425-1719
NSN 6610-01-412-4427
NSN 6220-00-548-1999
NSN 6320-00-242-3300
NSN 6105-01-392-0500
NSN 5835-00-723-2505
NSN 5895-01-178-6402
NSN 7035-01-245-2858
NSN 5998-00-322-9132
NSN 6105-00-370-3311
NSN 5975-00-947-1394