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SNCASE SE-2300

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.

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

Design and development edit

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]

Operational history edit

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]

Variants edit

SE-2300
Original version, two or three seats, conventional undercarriage.[2]
SE-2310
Three seats, tricycle undercarriage.[2] Two built, the second with faired undercarriage legs and wheels.[1][3]
SE-2311
Three seat, 101 kW (135 hp) Regnier 4L-00 engine.[4]

Specifications (SE-2300) edit

Data from Jane's All the World's Aircraft 1948[2]

General characteristics

  • Capacity: Two or three
  • Length: 7.40 m (24 ft 3 in)
  • Wingspan: 10.13 m (33 ft 3 in)
  • Height: 2.11 m (6 ft 11 in)
  • Wing area: 15.0 m2 (161 sq ft)
  • Empty weight: 685 kg (1,510 lb) equipped
  • Gross weight: 1,015 kg (2,238 lb)
  • Powerplant: 1 × Renault Bengali 4Pei 4-cylinder inverted air-cooled inline engine, 140 kW (190 hp) at 2,400 rpm
  • Propellers: 2-bladed, 1.90 m (6 ft 3 in) diameter wooden

Performance

  • Maximum speed: 235 km/h (146 mph, 127 kn)
  • Cruise speed: 212 km/h (132 mph, 114 kn)
  • Range: 900 km (560 mi, 490 nmi)
  • Service ceiling: 4,650 m (15,260 ft)
  • Wing loading: 67 kg/m2 (14 lb/sq ft)
  • Power/mass: 0.10 kW/kg (0.063 hp/lb)
  • Landing speed: 75 km/h (47 mph; 40 kn)
  • Landing distance: 300 m (985 ft) from 8 m (26 ft) with flaps down

References edit

  1. ^ a b c "SE-2300". Retrieved 17 November 2012.
  2. ^ a b c d e f g Bridgman, Leonard (1948). Jane's All the World's Aircraft 1948. London: Sampson, Low, Marston and Co. Ltd. p. 160c–161c.
  3. ^ a b "SE-2310". Retrieved 17 November 2012.
  4. ^ Gaillard, Pierre (1990). Les Avions Francais de 1944 à 1964. Paris: Éditions EPA. p. 34. ISBN 2 85120 350 9.

sncase, 2300, 2300, 2300, three, seat, wing, single, engine, touring, aircraft, built, just, after, world, france, 2310, tricycle, undercarriage, variant, neither, type, went, into, production, 2300se, 2310role, three, seat, tourernational, origin, francemanuf. 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 SE 2300SE 2310Role Two or three seat tourerNational origin FranceManufacturer Sud Est Societe nationale des constructions aeronautiques du Sud Est or SNCASE Designer Pierre SatreFirst flight 26 October 1945Number built 3 Contents 1 Design and development 2 Operational history 3 Variants 4 Specifications SE 2300 5 ReferencesDesign and development editPierre 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 Operational history editWith 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 Norecrin and development of the SE 2300 series was abandoned The last example remained in use until at least 1956 as a company hack 1 Variants editSE 2300 Original version two or three seats conventional undercarriage 2 SE 2310 Three seats tricycle undercarriage 2 Two built the second with faired undercarriage legs and wheels 1 3 SE 2311 Three seat 101 kW 135 hp Regnier 4L 00 engine 4 Specifications SE 2300 editData from Jane s All the World s Aircraft 1948 2 General characteristicsCapacity Two or three Length 7 40 m 24 ft 3 in Wingspan 10 13 m 33 ft 3 in Height 2 11 m 6 ft 11 in Wing area 15 0 m2 161 sq ft Empty weight 685 kg 1 510 lb equipped Gross weight 1 015 kg 2 238 lb Powerplant 1 Renault Bengali 4Pei 4 cylinder inverted air cooled inline engine 140 kW 190 hp at 2 400 rpm Propellers 2 bladed 1 90 m 6 ft 3 in diameter woodenPerformance Maximum speed 235 km h 146 mph 127 kn Cruise speed 212 km h 132 mph 114 kn Range 900 km 560 mi 490 nmi Service ceiling 4 650 m 15 260 ft Wing loading 67 kg m2 14 lb sq ft Power mass 0 10 kW kg 0 063 hp lb Landing speed 75 km h 47 mph 40 kn Landing distance 300 m 985 ft from 8 m 26 ft with flaps downReferences edit nbsp Wikimedia Commons has media related to SNCASE SE 2300 a b c SE 2300 Retrieved 17 November 2012 a b c d e f g Bridgman Leonard 1948 Jane s All the World s Aircraft 1948 London Sampson Low Marston and Co Ltd p 160c 161c a b SE 2310 Retrieved 17 November 2012 Gaillard Pierre 1990 Les Avions Francais de 1944 a 1964 Paris Editions EPA p 34 ISBN 2 85120 350 9 Retrieved from https en wikipedia org w index php title SNCASE SE 2300 amp oldid 1016832911, wikipedia, wiki, book, books, library,

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