| SE-2300 | |
|---|---|
 | |
| SE-2310 | |
| Role | Two or three seat tourer |
| National origin | France |
| Manufacturer | Sud-Est (Société nationale des constructions aéronautiques du Sud-Est or SNCASE) |
| Designer | Pierre Satre |
| First flight | 26 October 1945 |
| Number built | 3 |
The Sud-Est SE-2300 or S.N.C.A.S.E. SE-2300 was a two/three seat low wing, single engine touring aircraft, built just after World War II in France. The SE-2310 was a tricycle undercarriage variant. Neither type went into production.
Pierre Satre, who later was chief designer of the Concorde, began the SE-2300 design during World War II and it first flew on 26 October 1945. [1] It was a conventionally laid out, all metal, two seat, single engine cantilever monoplane, with tapered low wings having 4° of dihedral built around inverted U-section main and auxiliary spars. The wings had a centre section integral with the fuselage and two outer panels, all covered with electrically welded skin. There were plain flaps, with a maximum deflection of 40°. [2]
The fuselage of the SE-2300 was constructed from four pre-formed panels welded together. A 140 hp (104 kW) Renault Bengali 4 four cylinder, inverted, air-cooled inline engine, fed from a fuselage tank, drove a two blade propeller. The over-wing cabin seated two side-by-side with dual controls. Behind these seats was space for a third (optional in the SE-2300 and standard in the SE-2310 variant) and baggage. There were access doors and rear view transparencies on both sides. At the rear, the tailplane was mounted at mid-fuselage and the fin and deep rudder were straight tapered except near the keel and almost triangular above the fuselage. [2]
The first and only SE-2300 had a fixed conventional undercarriage with oleo-pneumatic springing, faired main legs and wheels and a swivelling tailwheel. [2] The two SE-2310s had tricycle undercarriages, the first unfaired [2] but the second with faired legs and spats. [3]
With a four-seat version, the SE-2311 under development but unbuilt, the three seat SE-3010 was entered into a 1946 French Transport Ministry contest for a four-seat tourist aircraft in February 1946. It was not successful, the award going to the Nord 1200 Norécrin and development of the SE-2300 series was abandoned. The last example remained in use until at least 1956 as a company hack. [1]
Data from Jane's All the World's Aircraft 1948 [2]
General characteristics
Performance
The Agusta A.101 was a large prototype transport helicopter developed in Italy during the 1960s. Despite prospective orders from the Italian armed forces, no buyers emerged and the project was abandoned in 1971.
The Chrislea Super Ace is a 1940s British four-seat light aircraft built by Chrislea Aircraft Limited.
The Ikarus 451 is a family of research aircraft designs built in Yugoslavia in the 1950s, all sharing the same basic airframe, but differing in powerplants and cockpit arrangements. One member of the family Ikarus 451M became the first domestically-built jet aircraft to fly in Yugoslavia, on 25 October 1952.
The BFW M.27, sometimes known as the Messerschmitt M.27, was a German two-seat sports plane with a low, cantilever wing, open cockpits and a fixed undercarriage sold in small numbers at the start of the 1930s.
The SNCAC Chardonneret were a short series of 1940s French three- and four-seat cabin monoplanes with the same wings and general layout but with different engines.
The Breda Ba.79S was a single-engine four-seat high-wing private aircraft built in Italy in the late 1930s. Only a few were produced.
The CANT Z.1012 was a small three-engined monoplane built in Italy in the late 1930s to carry either three or five passengers depending on the engines. A small number were built for Italian diplomatic use.
The Pasotti F.6 Airone was a low-wing, twin-engined, wooden, four seat civil aircraft built in Italy in the 1950s. Production was considered but only one was completed.
The Johansen CAJO 59 was a Danish twin-engined amphibious flying boat. Built in the late 1960s, it achieved certification but did not go into production.
The IAR-22 was a single engine basic trainer built in Romania in about 1934. It was a low-wing monoplane with two seats in tandem and a fixed conventional undercarriage.
The CNA Eta was a single engine Italian light aircraft, flown in the mid-1930s, that set one and two seat world records as both a landplane and a seaplane. Only one or two were built.
The CANSA C.4 was a single engine, open cockpit, tandem seat training aircraft and tourer flown in Italy in 1942.
The SAIMAN LB.2 was an unconventional Italian two seat cabin side by side sport aircraft designed around 1937, with a single pusher configuration engine, twin tail booms and an early tricycle undercarriage.
The Starck AS-80 Holiday is a conventional two-seat, single-engine high-wing monoplane designed and built in France around 1950. It was sold in kit form but only a few were completed.
The Waterman Arrowbile is a tailless, two-seat, single-engine, pusher configuration roadable aircraft built in the US in the late 1930s. One of the first of its kind, it flew safely but generated little customer interest, and only five were produced.
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 Bloch MB.90 was the first all-metal French light aircraft. Only two aircraft were completed, making their first flights in 1932, though there were several variants.
The SNCASE SE-700 was a three-seat passenger autogyro designed during World War II. Two were completed but only the first flew and the programme was soon abandoned.
The Caudron C.530 Rafale was a French two seat competition aircraft. Only seven were built but they had great success in several contests during 1934.
The Moskalyev SAM-10 was a late 1930s Soviet light transport aircraft suited to passenger or ambulance roles. Despite proving outstanding in trials, engine supply curtailed its production.
