2840-21-856-0437

Aircraft Gas Turbine Engine

2840218560437 218560437 GG4A2 544027 CD660138ITEM1B3

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. View more Aircraft Gas Turbine Engine

Managed by Canada

NSN Created on 23 Jul 1969

Data Last Changed
January 2023

NATO Update Count
1

NATO Data Quality

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