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 5855-01-188-4049
NSN 5905-01-252-9007
NSN 6135-01-351-1131
NSN 5915-01-085-6528
NSN 6645-01-557-4608
NSN 6685-01-555-7938
NSN 5855-00-482-9876
NSN 5905-00-523-0191
NSN 6145-01-320-5000
NSN 6610-01-567-3026
NSN 5915-00-197-0874
NSN 5965-00-393-1294