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Turbomeca Marboré

From Alfawiki
Turbomeca
Company typeCompany
IndustryAerospace, Aircraft engines
Founded1938 in France
Headquarters
France
ProductsTurbojet engines, including Marboré series

The Turbomeca Marboré is a compact turbojet engine developed and manufactured by Turbomeca during the period spanning the 1950s through the 1970s. Its main installations were on aircraft such as the Fouga CM.170 Magister and the Morane-Saulnier MS.760 Paris. In the United States, production was licensed under the designation Teledyne CAE J69. Additionally, in Spain, ENMASA built the Marboré II variant under license, naming it the Marboré M21.

Limited production characterized early models including Marboré I, III, IV, and V. The engine typically weighs approximately . When comparing fuel consumption at , the Marboré VI uses , whereas the Marboré II consumes , representing a 27% increase in fuel usage but offering enhanced thrust and operational efficiency.

Variants

Marboré I
Initial prototype and experimental units.
Marboré II
The first extensively produced model delivering maximum thrust of at 22,500 rpm. It employs a single-spool configuration with a centrifugal compressor and has a fuel consumption rate of . Differences among variants include military versus civilian adaptations, oil reservoir designs, auxiliary systems, and exhaust configurations. Some versions incorporate an axial compressor stage to boost performance.
Marboré IIA
Marboré IIB
Marboré IIC
Marboré IIF
Marboré IIG
Marboré III
Marboré IV
Marboré V
Marboré VI
Provides an increased thrust output of , approximately 23% higher than the Marboré II, with fuel consumption rising modestly by 9% to . This combination made it suitable for upgrading aircraft originally equipped with Marboré II engines, especially as surplus Marboré II units became available at lower costs.
Teledyne CAE J69: American licensed production and further development.
Marboré VIC
Marboré VIF

Applications

Marboré
J69
Refer to Teledyne CAE J69

References

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989.

External links