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 5950-00-279-3098
NSN 5905-01-130-8975
NSN 6620-01-499-1492
NSN 2925-00-708-4332
NSN 4140-00-185-9694
NSN 5915-01-464-0491
NSN 5925-00-229-3519
NSN 4140-01-188-0111
NSN 5965-01-367-6483
NSN 6105-01-207-8332
NSN 6135-01-142-6456
NSN 6130-01-498-1783