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 7035-01-092-5723
NSN 5905-00-289-0420
NSN 6135-01-156-4627
NSN 5835-01-608-8868
NSN 5950-01-382-9337
NSN 7035-01-441-8363
NSN 5945-01-159-1851
NSN 6610-00-531-8871
NSN 5950-01-449-3502
NSN 7035-01-489-5679
NSN 5999-01-200-0989
NSN 6240-00-684-8181