Morane-Saulnier M.S.755 Fleuret
1953
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Morane-Saulnier M.S.755 Fleuret

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Specification 
 MODELMS.755
 CREW2
 ENGINE2 x 400kg Turbomeca Marbore II turbojet
 WEIGHTS
    Take-off weight3024 kg6667 lb
    Empty weight1940 kg4277 lb
 DIMENSIONS
    Wingspan10.30 m34 ft 10 in
    Length9.70 m32 ft 10 in
    Height2.60 m9 ft 6 in
    Wing area18.00 m2193.75 sq ft
 PERFORMANCE
    Max. speed710 km/h441 mph
    Cruise speed614 km/h382 mph
    Ceiling11000 m36100 ft
    Rate of climb1020 m/min3350 ft/min
    Range725 km451 miles

Comments
Barry, 12.05.2016

This was "one off" jet trainer which was not accepted by the L'Armee de l'Aire, but did go undergo extensive tests with the Indian Air Force between March and June 1954, and as is so very often the case with India the air force liked it but no order was forthcoming. I suppose not enough palms were greased. However the MS 755 did form the basis for the more successful Paris.

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