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The MS.250 was a parasol-wing monoplane with swept-back wings, similar to the Morane-Saulnier MS.230, but differed in having a new tail. The cockpits had windscreens, and the rear cockpit had a gun ring. The pilot-instructor manned the front cockpit, and the trainee observer manned the rear cockpit. [1]
Although MS vary in many aspects, structures and functions, all the MS studied to date share an important feature: in a process called gating, they all open in a pore-like manner when protein channels are activated by a mechanical stimulus. There are currently two models of the gating process that explain how membrane-activated ion channels open.
A MS.880B Rallye Club. The SOCATA Rallye is a single-engined, low-wing monoplane light aircraft, capable of STOL (short takeoff and landing) performance. The Rallye is considered to be sound and functional aircraft; efforts were made upon later-built aircraft to improve the type's visual appeal and to clean up the exterior. [19]
The engine was replaced with a German war-surplus 240 hp (180 kW) Argus As 10 and the prototype flew again in November 1949 as the MS.731. Two further prototypes were built and flown in 1951 designated MS.732 , they were each powered by a Potez 6D 02 engine and the original fixed landing gear of the prototype was replaced with retractable main ...
MS.234/2 converted from MS.130 Coupe Michelin racer with 172 kW) (230 hp) Hispano 9Qb and NACA cowling, entered in 1931 Coupe Michelin air race, 86 kW (250 hp) Hispano-Suiza 9Qa engine. [10] Fitted with a Hispano-Suiza 9Qa engine as MS.234 #2, flown in aerobatic competition by Michael Detroyat until 1938. [11] MS.235
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In response to a requirement for a fighter issued by the French Air Force in 1934, Morane-Saulnier built a prototype, designated MS.405, of mixed materials. This had the distinction of being the company's first low-wing monoplane, as well as the first to feature an enclosed cockpit, and the first design with a retracting undercarriage .
RFC Morane-Saulnier N. While the Type N was a clean, streamlined aircraft, it was not easy to fly due to a combination of stiff lateral control caused by using wing warping instead of ailerons, sensitive pitch and yaw controls caused by using an all flying tail, and very high landing speed for the period.