2840-25-134-1817
Aircraft Gas Turbine Engine Combustion Chamber
2840251341817 251341817
The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case. View more Aircraft Gas Turbine Engine Combustion Chamber
Managed by Norway
Data Last Changed
January 2024
January 2024
NATO Update Count
1
1
NATO Data Quality
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