The Morane-Saulnier M.S.225 was a French fighter aircraft of the 1930s. It was produced in limited quantities to be used as a transitional aircraft between the last of the biplanes and the first monoplane fighters.
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Design and development.
The M.S.225 was a parasol monoplane, with a wide fixed landing gear, and powered by a Gnome-Rhône 9Krsd radial engine. Having a circular fuselage the M.S.225 was much more robust than its immediate predecessor, the M.S.224.
Created as a stop-gap before the introduction of more advanced aircraft still under development, the Morane-Saulnier M.S.225 was first shown in the form of a model at the Paris Air Show of 1932. After successful flight tests of the prototype, series production started at once.
Classified in the category C.1 (single-seat fighter), 75 aircraft were produced. A total of 53 aircraft were delivered to the Air Force in November 1933. The "Aéronavale" received the first of the 16 aircraft it had ordered in February 1934. Three were also sold to China.
Operational history.
The M.S.225s of the "Armée de l'Air" served in the "7e Escadre de Chasse" (7th Fighter Wing) at Dijon, and in two "escadrilles" of the "42e Escadre" (42nd Wing), based at Rheims. They were withdrawn from front-line service between 1936 and 1937. The aircraft also flew with the "Aéronavale l'Escadrille 3C1", established in Marignane, this formation later transferring to the Air Force at the beginning of 1936, where it became "Le Groupe de Chasse II/8".
The Air Force Aerobatic Squadron based at Étampes used five modified M.S.225s, with a larger vertical stabilizer, while the last unit of the Air Force to operate this aircraft was the flying school based at Salon-de-Provence.
At the outbreak of World War II, only 20 M.S.225s were still in flying condition, the majority of them being scrapped in mid-1940.
Production variant with a Gnome-Rhone 9Krs engine, 75 built.
Variant fitted with an arrestor hook in 1933 for aircraft carrier operations, powered by a Gnome &amp; Rhône 9Kdr.
Variant of the 226 with folding wings first flown in 1934.
Variant used as test bench for the 515 kW (690 hp) Hispano-Suiza 12Xcrs engine, with a four-bladed propeller. 
First flying in 1934, this version had a modified aerofoil and empennage, and was powered by a 515 kW (690 hp) Gnome-Rhône 9Krse; did not enter production. 
Conversion of the M.S.225 equipped with a 388 kW (520 hp) Clerget 14Fcs diesel engine.
Specifications (M.S.225).
"Data from" "The Complete Book of Fighters"General characteristics* Crew: 1* Aspect ratio: * Propellers: 2-bladed fixed-pitch wooden propeller
Performance* Endurance: * g limits: * Roll rate: * Time to altitude: in 5 minutes 42 seconds
Armament
See also.
Aircraft of comparable role, configuration, and era
Related lists
References.
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