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Morane-Saulnier MS.230
↑ Morane-Saulnier MS.230 History
World War 1 (1914-1918) allowed the French to become globally-recognized leaders in military aviation, resulting in many classic types emerging from French aero-concerns such as Breguet, Caudron, Nieuport, SPAD, and others. This market recognition continued into the post-war period (known as the Interwar period) and resulted in other successful entries like the Morane-Saulnier MS.230 of the late-1920s.
The MS.230 was developed to fulfill a basic trainer role and accomplished this through simple construction and equally-simple controlling to go along with inherent stability. Over 1,000 examples were produced by Morane-Saulnier and the primary operator became the French military flying school at Reims. Global operators proved numerous and ranged from Belgium and Brazil to the United States (under the USAAC) and Venezuela. For the French, the MS.230 served as its primary trainer throughout most of the 1930s which covered the lead-up to World War 2 (1939-1945).
At least six aircraft were built to the MS.231 standard of 1930 which instead carried the Lorraine 7Mb engine of 240 horsepower. The MS.232 was a one-off experimental model of 1930 and powered by the Clerget 9Ca diesel-fueled engine of 200 horsepower output. The MS.233 followed and fitted either the Gnome-Rhone 5Ba or 5Bc engine types of 230 horsepower - sixteen went to Portugal and a further six examples stayed in France. The MS.234, numbering two examples, carried the Hispano-Suiza 9Qa of 20 horsepower. The MS.234/2 was an offshoot of the line built from the MS.130 Couple Michelin racing aircraft. This form was given the Hispano 9Qb under a racing-style engine cowling and flown at various levels up until 1938.
The MS.235 was a single example of 1930 powered by the Gnome-Rhone 7Kb engine of 300 horsepower. The MS.235H added floats for on-water landings and take-offs and saw its first flight in 1931. The MS.236, first-flying in 1932, were nineteen aircraft built for the Belgian Air Force and powered by an Armstrong Siddeley "Lynx" ICV series engine. The MS.237 of 1934 rounded out the MS.230 family line as a group of five airframes powered by the Salmson 9Aba engine of 280. These were purchased and flown in private hands.
In Czech Air Force service, the MS.230 was designated as the "C.23". The pre-World War 2 German Luftwaffe operated this French aircraft as well but only in limited numbers.
↑ Morane-Saulnier MS.230 Specification
↑ BASICS
Year:
1929
Status:
Retired, Out-of-Service
Crew:
2
↑ MANUFACTURING
[ 1,005 Units ]:
Morane-Saulnier - France
↑ ROLES
- Training
↑ DIMENSIONS
Length:
21.98 ft (6.7 m)
Width/Span:
35.10 ft (10.7 m)
Height:
9.19 ft (2.8 m)
↑ WEIGHTS
Empty Weight:
1,830 lb (830 kg)
MTOW:
2,535 lb (1,150 kg)
(Diff: +705lb)
↑ POWER
1 x Salmson 9AB 9-cylinder air-cooled radial piston engine developing 230 horsepower driving a two-bladed propeller at the nose.
↑ PERFORMANCE
Maximum Speed:
162 mph (260 kph; 140 kts)
Service Ceiling:
16,404 feet (5,000 m; 3.11 miles)
Maximum Range:
360 miles (580 km; 313 nm)
↑ ARMAMENT
None.
↑ VARIANTS
MS.230 - Base Series Designation; definitive production model.
MS.229 - Fitted with Hispano-Suiza 8a V8 engine; two examples completed.
MS.231 - Fitted with Lorraine 7Mb engine of 240 horsepower; six completed.
MS.232 - One-off experimental variant fitted with Clerget 9Ca diesel-fueled engine of 200 horsepower.
MS.233 - Fitted with Gnome-Rhone 5Ba OR 5Bc engine of 230 horsepower; 22 completed with sixteen built under license in Portugal.
MS.234 - Fitted with Hispano-Suiza 9Qa engine; two examples completed.
MS.234/2 - MS-130 racer model converted with Hispano 9Qb engine of 230 horsepower under new racing cowling.
MS.235 - Fitted with Gnome-Rhone 7Kb engine of 300 horsepower; single example of 1930.
MS.235H - Float-equipped variant of 1931.
MS.236 - Fitted with Armstrong-Siddeley Lynx ICV engine of 215 horsepower; model of 1932; license production by Belgium.
MS.237 - Fitted wit Salmson 9Aba engine of 280 horsepower; model of 1934; five complete for private buyers.
