Sud-Ouest SO.1120 Ariel III

The 1948 experimental Ariel helicopters used tip jets at the blade tips.

The SO.1221 was powered by a cold-jet propulsion system developed by Sud-Ouest for its earlier two prototypes Ariel II and III helicopters. Residual thrust from the engine is ducted to the end of the fuselage and used for directional control.

Engine: 275 h.p. Turbomeca Arrius gas-turbine
Rotor diameter: 35 ft 5 in
Rotors: 3-blade tip-powered main rotor.
Fuselage length: 27 ft 2 in
Loaded weight: 2,750 lb
Ceiling: 15,000 ft
Typical range: 155 miles at 85 mph with 1,000 lb load
Seats: 2-3

Sud-Ouest SO-1119 Ariel II

The 1949 Sud-Ouest SO-1119 Ariel II was the first French reaction jet helicopter to fly. Rotor tip jets were fed by an exhaust-driven compressor driven by a 190-hp Mathis C-40 located in the fuselage.

The SO-1119 Ariel II is at the French Musee de L’Air.

Engine: Mathis C-40, 190 hp
Rotor diameter: 35,42 ft
Fuselage length: 23.39 ft
Max speed: 102 mph
ROC: 1082 fpm

Sud-Ouest / Ouest Aviation

France
Formed 1935 at Bordeaux-Merignac by the Potez group when it took over the Societe Aerienne Bordelaise. Was intended as a decentralized production source for Potez and Bloch aircraft. A prime responsibility was development and production of Bloch types, especially single-seat fighters derived from MB.150 of 1936. Redesign facilitated production and improved performance, resulting in MB.151 and 152. By June 1940 production totaled about 600, involving five plants. MB.175 twin-engined bomber was in production and was revived after Second World War as torpedo aircraft. Several other prototypes built, including four-engined bomber.

In France, the Socialist Government of the so called Popular Front brought all the companies building military aircraft, aero engines and ar¬mament under its control in 1936. The im¬mediate result was the socialized oblivion of such established companies as Marcel Bloch, Bleriot, Nieuport, Potex, Dewoitine, Hanriot and Farman within half a dozen nationalized groups or Societies Nationales, named ac¬cording to their geographical location (Nord, Ouest, Centre, Midi and so on).

Incorporated in SNCASO 1936, incorporating the factories of Marcel Bloch, Bleriot and Liore et Olivier, subsequently merging with SNCASO and changing name to Ouest Aviation in 1956.

In 1942 completed forerunner of Bretagne twin-engined transport, though not flown until 1945; then used commercially and experimentally. Numerous and varied post-Second World War types included distinctly unusual forms of rotary-wing aircraft. Aeriel (1948) and Djinn (1953) with tip jets, and Farfadet convertiplane (1953).

Aerocentre went into liquidation during 1949, its plants and work being shared by SNCAN (Nord), SNCASO (Sud-Ouest) and engine form SNECMA.

Original designs included S.O.94R twin-engined trainer; S.O.95 Corse, and S.O.30 Bretagne military transports; S.O.4050 Vautour twin-jet bomber; and the S.O.9000 Trident. The S.O.1221 Djinn two-seat helicopter was produced, and Vertol H-21 helicopters were manufactured under license for the French Army. Ouest became part of Aerospatiale.

After World War II, although four of the nationalized groups continued operating un¬der state control, private companies were al¬lowed to resume the design and manufacture of both civil and military aircraft. Some of the pioneering names of French aviation, such as Breguet and Morane Saulnier, returned to prominence, and by 1950 a new one had been added Avions Marcel Dassault.

Loire-Nieuport joined SNCASO in 1942.

SNCASO and SNCASE joined to form Sud-Aviation in 1958.

Sud-Est SE 3130 Alouette II

The Alouette II is a turbine development of the earlier SE-3120 Alouette with 200 h.p. Salmson 9 NH piston engine. A small pre-production batch was under construction, with the first five due for delivery late 1955.

Engine: Turbomeca Artouste II turbine, 360 hp
Rotors: 3-blade main; 2-blade tail
Rotor diameter: 38 ft
Loaded weight: 2,980 lb
Ceiling: 14,764 ft
Typical range: 323 miles at 106 mph
Seats: 5

Sud-Est SE-3120 Alouette

SE.3120

The Sud-Est SE 3120 Alouette (Lark) a three seat light helicopter was designed mainly for agricultural purposes. The first of two prototypes (F-WGGD and -WGGE) was flown on 31 July 1952, powered by a 149kW Salmson 9NH radial engine with an articulated three-blade rotor. Its rotor has three degrees of freedom: pitch, in-plane motion and vertical flapping. Pitch is controlled by means of a stabilizing gyroscope.

In July 1953, established a new international helicopter closed-circuit duration record of 13 hours 56 minutes. Two other prototypes followed, one of which was a three-seater.

It was the first of the successful Alouette family of helicopters.

The basic airframe of the Sud-Est SE-3120 Alouette was completely redesigned to take the 269kW Turbomeca Artouste II turboshaft, and the first of two prototypes, designated SE 3130, was flown on 12 March 1955.

Sud-Est SE.3120
Engine: 1 x Salmson 9NH, 150kW
Main rotor diameter: 11.60m
Length: 10.45m
Max take-off weight: 1150kg
Empty weight: 750kg
Max speed: 125km/h
Service ceiling: 4000m
Range: 225km

Sud-Est SE.3110

SE.3110

After the Sud-Est SE.3101, followed the 2-seat SE.3110 (F-WFUE), which had a 200hp Salmson 9 NH piston engine.

The 1947 Sud-Est SE.3110 helicopter still relied on the twin-tail rotor system used in the experimental SE.3101, which acted against torque and for directional and longitudinal control, and an enclosed cabin seating two side-by-side.

Sud-Est SE.3110
Engine: 1 x Salmson 9NH, 150kW
Main rotor diameter: 12m
Length: 11.13m
Max take-off weight: 950kg
Empty weight: 670kg
Max speed: 160km/h
Cruising speed: 115km/h
Rate of climb: 244m/min
Service ceiling: 4500m
Range: 300km

Sud-Est SE.3101

SE.3101

The first all-French helicopter to be designed and built after World War 2, SNCA du Sud-Est’s single-seat SE.3101 was powered by an 85hp Mathis engine and flew for the first time on 1 June 1948.

This experimental helicopter was to study the placing of auxiliary rotors intended simultaneously to provide torque correction and longitudinal control. Two rotors, with compressed wood blades 1.6m in diameter, were placed symmetrically at 45°, one on each side of a V-shaped beam at the end of the fuselage, which was made of soldered tubes without a skin covering. These variable-pitch airscrews enabled the aircraft to be steered by varying their pitch differentially.

There then followed the 2-seat SE.3110 (F-WFUE), which had a 200hp Salmson 9 NH piston engine.

SE.3101

Sud-Est SE.3101
Engine: 1 x Mathis 4GB 20, 82kW
Main rotor diameter: 7.50m
Length: 6.90m
Max take-off weight: 520kg
Empty weight: 400kg
Max speed: 120km/h
Cruising speed: 95km/h
Service ceiling: 3000m
Range: 100km

Sud-Est

Societe Nationale de Constructions Aeronautiques du Sud-Est
SNCASE

In France, the Socialist Government of the so called Popular Front brought all the companies building military aircraft, aero engines and ar¬mament under its control in 1936. The im¬mediate result was the socialized oblivion of such established companies as Marcel Bloch, Bleriot, Nieuport, Potex, Dewoitine, Hanriot and Farman within half a dozen nationalized groups or Societies Nationales, named ac¬cording to their geographical location (Nord, Ouest, Centre, Midi and so on). Liore-et-Olivier, Potez, Romano, and SPCA formed SNCASE in 1936. Sud-Est was a nationalised company that had taken over manufacture from Bloch.

Company thus became responsible for development and production of LeO.45 twin-engined bomber, first flown January 1937, outstanding in many points of design and much used and adapted during and after Second World War. Built also Romano trainers and LeO.43 catapult floatplane, of type first flown December 1934.

In 1941 the company absorbed SNCAM. Early post-Second World War products included Languedoc four-engined airliner, developed from Bloch 161 of 1939, which entered service between Paris and Algiers in 1946, and was ordered additionally for military use.

Dewoitine joined SNCASE in 1942.

After World War II, although four of the nationalized groups continued operating un¬der state control, private companies were al¬lowed to resume the design and manufacture of both civil and military aircraft. Some of the pioneering names of French aviation, such as Breguet and Morane Saulnier, returned to prominence, and by 1950 a new one had been added Avions Marcel Dassault.

Military types in development included Grognard twin-jet attack aircraft of 1950; the unique trolley-launched skid-landing Baroudeur strike aircraft of 1953; and Mistral and Aquilon developments of the British de Havilland Vampire and Sea Venom. Especially notable original developments were the Alouette helicopter series first flown in 1951, and the rear-engined twin-jet Caravelle in 1955.

Until 1 September 1956 known as Societe Nationale de Constructions Aeronautiques du Sud-Est (SNCASE). On the 1st September 1956 the S.N.C.A. du Sud-Est was merged with the S.N.C.A. du Sud-Oest into Sud-Aviation.

Sud-Aviation SE.3131 Gouverneur

This new helicopter, which was brought out as a product of Sud Aviation, first flew on 10 May 1957 (F-WIEA). It was introduced to the public during the French International Air Show at le Bourget soon afterwards. It basically an Alouette II with an Artouste engine, covered fuselage and executive cabin seating 5 occupants including the pilot, by the well-known expert Loewy.

Streamlining gave the Gouverneur improved cruising speed.

Both the main and the anti-torque rotor are taken from the Alouette, but to protect the latter, a bow-shaped tail skid is provided. Much thought has been given to making the Gouverneur’s cabin as comfortable as possible, particularly by means of sound-proofing.

Engine: 1 x Turbomeca Artouste II
Rotor diameter: 10.2m
Length: 9.7m
Fuselage width: 2.08m
Gross weight: 1500kg
Empty weight: 925kg
Cruising speed: 195km/h
Absolute ceiling: 4600m
Range: 600km
Seats: 5

Sud-Aviation

Formed 1 March 1957 by amalgamation of Ouest-Aviation (SNCASO) and Sud-Est Aviation (SNCASE). Main responsibility was further development and marketing of highly successful S.E.210 Caravelle twin-jet airliner, first flown in 1955, and Alouette series of helicopters. Continued also development of S.E.5000 Baroudeur, S.O.9050 mixed-power interceptor and widely used S.O.4050 Vautour twin-jet multipurpose aircraft. Frelon series of large turbine-powered helicopters developed after first flight in February 1959, and Super Frelon flew December 1962, setting new world records. In 1965, Morane-Saulnier became a subsidiary of Sud-Aviation. Design leadership in A300 European Airbus assumed and diversification into non-aeronautical fields undertaken. Jointly with Nord Aviation made Corvette light rear-engined jet transport.

On January 1st, 1970 became major component of Aerospatiale, with Nord-Aviation and SOCATA, and the missile manufacturing company, SEREB.