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Morane-Saulnier M.S.325
The M.S.325 was a French Armée de l'Air fighter aircraft built by Morane-Saulnier in 1933 to meet the requirements of 1930 fighter aircraft specification. The design was unsuccessful and was abandoned in 1934.
==Design and development==
In 1930, when the Jockey ''legier Chasse'', or ''Plan Caquot'' light weight fighter program was judged a failure, the Service Technique de l' Aeronautique issued the C1 (monoplace de chasse) requirement. C1 (upgraded on 26 January 1931) called for a single-seat fighter powered by a supercharged engine with a cylinder capacity of between . Ultimately no fewer than 10 designs and 12 prototypes were offered, all designed around the Hispano-Suiza 12Xbrs developing at , with proven reliability and a relatively small frontal area. The Morane-Saulnier submissions included the M.S.275 which retained the classic parasol monoplane configuration of preceding Morane-Saulnier fighters. In the more innovative M.S.325, a low wing, duralumin-skinned all-metal configuration was employed.
The M.S.325 was relatively modest in its concept still featuring an open cockpit (originally the tail surfaces were fabric covered) and fixed-gear with the semi-elliptical two-spar wings braced by exterior struts. The wings had two jettisonable wing root fuel tanks with a pair of Châtellerault machine guns mounted one above each of the widely spaced landing gear legs. More unusual was that the incidence of the starboard wing greater than that of the port wing to counter torque; the engine was also canted slightly to port to counter the resultant yaw.〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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