"},"prime units?":{"wt":"met\n"},"genhide":{"wt":""},"crew":{"wt":""},"capacity":{"wt":""},"length m":{"wt":"16.35"},"length ft":{"wt":""},"length in":{"wt":""},"length note":{"wt":""},"span m":{"wt":"21.75"},"span ft":{"wt":""},"span in":{"wt":""},"span note":{"wt":""},"height m":{"wt":""},"height ft":{"wt":""},"height in":{"wt":""},"height note":{"wt":""},"wing area sqm":{"wt":""},"wing area sqft":{"wt":""},"wing area note":{"wt":""},"airfoil":{"wt":""},"empty weight kg":{"wt":""},"empty weight lb":{"wt":""},"empty weight note":{"wt":""},"gross weight kg":{"wt":"5461"},"gross weight lb":{"wt":""},"gross weight note":{"wt":""},"max takeoff weight kg":{"wt":""},"max takeoff weight lb":{"wt":""},"max takeoff weight note":{"wt":""},"more general":{"wt":""},"eng1 number":{"wt":"4"},"eng1 name":{"wt":"[[Renault 6Q]]"},"eng1 type":{"wt":"six-cylinder inline inverted piston engine"},"eng1 kw":{"wt":""},"eng1 hp":{"wt":"240"},"eng1 note":{"wt":""},"power original":{"wt":""},"thrust original":{"wt":""},"prop blade number":{"wt":""},"prop name":{"wt":""},"prop dia m":{"wt":""},"prop dia ft":{"wt":""},"prop dia in":{"wt":""},"prop note":{"wt":""},"perfhide":{"wt":""},"max speed kmh":{"wt":"340"},"max speed mph":{"wt":""},"max speed kts":{"wt":""},"max speed note":{"wt":""},"max speed mach":{"wt":""},"cruise speed kmh":{"wt":""},"cruise speed mph":{"wt":""},"cruise speed kts":{"wt":""},"cruise speed note":{"wt":""},"stall speed kmh":{"wt":""},"stall speed mph":{"wt":""},"stall speed kts":{"wt":""},"stall speed note":{"wt":""},"never exceed speed kmh":{"wt":""},"never exceed speed mph":{"wt":""},"never exceed speed kts":{"wt":""},"never exceed speed note":{"wt":""},"minimum control speed kmh":{"wt":""},"minimum control speed mph":{"wt":""},"minimum control speed kts":{"wt":""},"minimum control speed note":{"wt":""},"range km":{"wt":""},"range miles":{"wt":""},"range nmi":{"wt":""},"range note":{"wt":""},"endurance":{"wt":""},"ceiling m":{"wt":""},"ceiling ft":{"wt":""},"ceiling note":{"wt":""},"climb rate ms":{"wt":""},"climb rate ftmin":{"wt":""},"climb rate note":{"wt":""}},"i":0}}]}" id="mwNQ">Data from French Postwar Transport Aircraft [1]
General characteristics
Performance
The SNCASE S.E.2010 Armagnac was a large French airliner of the late 1940s built by SNCASE (Sud-Est). The aircraft's disappointing performance and range prevented it from achieving commercial success. Although the SNCASE Armagnac did not have a sterling career, its passenger compartment design gave it a much roomier feel and greater capacity and foreshadowed the future wide-body jet airliners.
The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211. The design added two features, a pressurized cooling system that required considerably less cooling fluid which allowed the engine to be built smaller and lighter, and a number of improvements that allowed it to run at higher RPM. These changes boosted power by over 500 hp and made the 213 one of the most sought-after Axis engine designs in the late-war era.
The Sud-Ouest S.O.30 Bretagne was a 1940s French airliner built by Sud-Ouest.
The Latécoère 631 was a civil transatlantic flying boat built by Latécoère, the largest ever built up to its time. The type was not a success, being unreliable and uneconomic to operate. Five of the eleven aircraft built were written off in accidents and one was lost during World War II.
The Fouga CM.10 was an assault glider designed for the French Army shortly after World War II, capable of carrying 35 troops, later converted as a powered transport.
The Hurel-Dubois HD.31, HD.32, and HD.34 were a family of civil aircraft produced in France in the 1950s, based on Maurice Hurel's high-aspect ratio wing designs.
The SNCASE SE.161 Languedoc was a French four-engined airliner produced by SNCASE (Sud-Est). Developed from the Bloch MB.160 and known in the late 1930s as the (SNCSO) Bloch MB.161, the SE.161 was in service with Air France and the French military after World War II.
The SNCAC Martinet was a German-designed but French-built twin-engined military trainer and light transport monoplane. It was operated by the French military and in small numbers by French airlines from the late 1940s.
The SNCAC NC.211 Cormoran was a large four-engined military transport aircraft for passengers and cargo designed and built by SNCAC from 1945.
The Sud-Ouest Corse was a French mail and passenger transport aircraft, built by SNCASO.
The Nord 2100 Norazur was a 1940s French military transport monoplane designed and built at Courbevoie near Paris by SNCAN.
The Bréguet 890 Mercure was a late 1940s French cargo and passenger transport aircraft designed by Bréguet Aviation. Three variants were produced including a military variant called the Mars but none entered production.
The Dewoitine HD.730 was a prototype French reconnaissance floatplane of the 1940s. It was a single-engined, low-wing monoplane that was designed as a catapult-launched reconnaissance aircraft to operate from warships of the French Navy. Two flew in 1940, and a third aircraft was built to a modified design in 1941, but no production followed.
The Nord 260, built in prototype form as the Max Holste MH.260 Super Broussard,, was a turboprop-powered, uprated version of the piston-engined Max Holste MH.250 Super Broussard, that was further developed into the Aérospatiale N 262.
The Sud-Est or SNCASE SE-2100, sometimes known as the Satre SE-2100 after its designer, was a tailless, pusher configuration touring monoplane with a single engine and cabin for two. Only one was built.
The SIPA S.70 was a late 1940s French eight-passenger light transport aircraft prototype built by Société Industrielle Pour l’Aéronautique (SIPA).
The SNCASE SE-1010 was a late 1940s French photo-survey aircraft designed and built by SNCASE for the Institut Géographique National, one prototype was built but it crashed and the project was cancelled.
The Morane-Saulnier MS-700 Pétrel was a French four-seat cabin-monoplane designed and built by Morane-Saulnier, only three prototypes were built.
The SNCASO SO.7010 Pégase was a six-passenger light transport aircraft developed in France immediately after World War II. It was powered by a pair of tandem-coupled V-8 engines but this power plant proved to be too troublesome for development to proceed.
The Renault 6Q, also called the Renault Bengali 6, is an air-cooled inverted in-line six-cylinder, aircraft piston engine, producing about 160 kW (220 hp) continuous power. It was designed and built in France and produced for more than ten years after its homologation in 1936, with large numbers built during World War II.