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Turbomeca Marbore I

Turbojet with single-stage compressor, annular combustion chamber with rotating fuel delivery ring and single stage turbine. The Marbore was developed as a higher-powered version of the Pimene/Palas.

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Turboméca Marboré I. Source : Documentation Turboméca
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Turbomeca Marbore N°29 en essai chez Continental aux Etats-unis
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Turboméca Marboré I. Source : Flight, 29 june 1951
Dimensions
Diamètre..............60cm23.4inch
Longueur.............138cm54.2inch
Poids
Poids non équipé...120kg265lb.
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Poussée et consommation spécifique à la vitesse de croisière

List of Aircraft on which the "Marbore I" was installed

Leduc 016

The Leduc 016 was developed with wingtip mounted Marbore I