TURBOMECA MARBORÉ II ENGINE
The Turbomeca Marboré is a small turbojet engine that was produced by Turbomeca from 1950s to 1970s for training aircrafts. The most popular installations of this engine were in the Fouga CM.170 Magister and the Morane-Saulnier MS.760 Paris.
The first major production version was the Marboré II, which had a maximum thrust of 880 lb at 22,500 rpm. In its most basic form, it is a single-spool, centrifugal compressor turbojet.
Fuel consumption was rated at 410 l/h (110 gal/h). Variations include military or civilian aircraft, oil tank design, auxiliary equipment, and exhaust pipe configuration. Some variants also include one axial stage compressor for additional performance. The engine dimensions differ depending on the variant, auxiliary components and mounting configurations.
It was brought into M.S.Ö. Air & Space Museum with the contribution of Mr. Erol ÖZMAN.