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Nord Norécrin

The Nord 1200 Norécrin is a French two or three-seat (later four-seat) cabin monoplane designed and built by Nord Aviation.

1200 Norécrin
Nord 1203 Norécrin
Role Cabin monoplane
Manufacturer Nord Aviation
First flight 15 December 1945
Number built 378

Development edit

The Norécrin was developed to meet a French ministry of transport sponsored design competition. The Norécrin is a low-wing cantilever monoplane with a retractable tricycle landing gear and the prototype (Nord 1200) was designed to receive a nose-mounted 75 kW (100 hp) Mathis G4-R piston engine but flew only with a 100 kW (140 hp) Renault 4Pei (first flight on 15 December 1945 with Georges Detre as test pilot). The production version had three-seats and was designated the Nord 1201 Norécrin I. A number of variants were produced with different engines fitted. Later variants had four-seats and the Nord 1203 Norécrin V was a two-seat military variant with machine-guns and rockets. It was a successful design and 378 aircraft were built.

Variants edit

1200 Norécrin
Prototype with a 100 kW (140 hp) Renault 4Pei engine.
1201 Norécrin I
Three-seat production variant with a 100 kW (140 hp) Renault 4P-01 engine (22 built)
1202 Norécrin
Prototype four-seat variant with a 120 kW (160 hp) Potez 4D-01 engine
 
Nord 1203 Norecrin II at Sherburn-in-Elmet airfield, Yorkshire, in July 1951
1203 Norécrin II
Production variant with 101 kW (135 hp) Regnier 4L-00 engine.
1203 Norécrin III
Norécrin II with modified landing gear.
1203 Norécrin IV
Powered by a 130 kW (170 hp) Regnier 4L-02 engine.
1203 Norécrin V
Armed military variant.
1203 Norécrin VI
1955 production variant with a 120 kW (160 hp) Regnier 4L-14 engine.
1203 Norécrin M1
1955 prototype with a 130 kW (180 hp) Lycoming O-360 engine, derated to 120 kW (160 hp) .
1204 Norécrin
Powered by a 93 kW (125 hp) Continental C125 flat-four engine.
1204/II Norécrin
Powered by a 108 kW (145 hp) Continental C145-2 flat-four engine.

Operators edit

  Brazil
  • OMTA - One aircraft only.

Military operators edit

  Argentina
  France
  Israel
   Switzerland

Specifications (1203 Norécrin II) edit

 
Nord 1200 2-view drawing from L'Aerophile March 1946

Data from The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. p. 2616.

General characteristics

  • Crew: one
  • Capacity: three passengers
  • Length: 7.21 m (23 ft 8 in)
  • Wingspan: 10.22 m (33 ft 6.25 in)
  • Height: 2.90 m (9 ft 6 in)
  • Wing area: 13 m2 (139.93 sq ft)
  • Empty weight: 652 kg (1,437 lb)
  • Gross weight: 1,050 kg (2,315 lb)
  • Powerplant: 1 × Regnier 4L-00 air-cooled inverted inline piston-engine , 101 kW (135 hp)

Performance

  • Maximum speed: 280 km/h (174 mph, 151 kn)
  • Range: 900 km (559 mi, 486 nmi)
  • Service ceiling: 5,000 m (16,405 ft)

References edit

  1. ^ Aloni 2005, pp. 54–55
  • Aloni, Shlomo (September 2005). "Ils furent les deux premiers avions français de l'armée israélienne: Les deux "Norécrin d'Israël". Le Fana de l'Aviation (in French). No. 430. pp. 52–55.
  • Cuny, Jean (1989). Les avions de combat français, 2: Chasse lourde, bombardement, assaut, exploration [French Combat Aircraft 2: Heavy Fighters, Bombers, Attack, Reconnaissance]. Docavia (in French). Vol. 30. Ed. Larivière. OCLC 36836833.
  • Salatin, Claude (March 2002). "Courrier des Lecteurs" [Readers' Letters]. Avions: Toute l'Aéronautique et son histoire (in French) (108): 2. ISSN 1243-8650.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. p. 2616.
  • Le Trait d'Union (The Norecrin serie by Claude Salaun issue 109 to 121 1986-1988). French branch of Air Britain.


nord, norécrin, nord, 1200, norécrin, french, three, seat, later, four, seat, cabin, monoplane, designed, built, nord, aviation, 1200, norécrinnord, 1203, norécrinrole, cabin, monoplanemanufacturer, nord, aviationfirst, flight, december, 1945number, built, con. The Nord 1200 Norecrin is a French two or three seat later four seat cabin monoplane designed and built by Nord Aviation 1200 NorecrinNord 1203 NorecrinRole Cabin monoplaneManufacturer Nord AviationFirst flight 15 December 1945Number built 378 Contents 1 Development 2 Variants 3 Operators 3 1 Military operators 4 Specifications 1203 Norecrin II 5 ReferencesDevelopment editThe Norecrin was developed to meet a French ministry of transport sponsored design competition The Norecrin is a low wing cantilever monoplane with a retractable tricycle landing gear and the prototype Nord 1200 was designed to receive a nose mounted 75 kW 100 hp Mathis G4 R piston engine but flew only with a 100 kW 140 hp Renault 4Pei first flight on 15 December 1945 with Georges Detre as test pilot The production version had three seats and was designated the Nord 1201 Norecrin I A number of variants were produced with different engines fitted Later variants had four seats and the Nord 1203 Norecrin V was a two seat military variant with machine guns and rockets It was a successful design and 378 aircraft were built Variants edit1200 Norecrin Prototype with a 100 kW 140 hp Renault 4Pei engine 1201 Norecrin I Three seat production variant with a 100 kW 140 hp Renault 4P 01 engine 22 built 1202 Norecrin Prototype four seat variant with a 120 kW 160 hp Potez 4D 01 engine nbsp Nord 1203 Norecrin II at Sherburn in Elmet airfield Yorkshire in July 19511203 Norecrin II Production variant with 101 kW 135 hp Regnier 4L 00 engine 1203 Norecrin III Norecrin II with modified landing gear 1203 Norecrin IV Powered by a 130 kW 170 hp Regnier 4L 02 engine 1203 Norecrin V Armed military variant 1203 Norecrin VI 1955 production variant with a 120 kW 160 hp Regnier 4L 14 engine 1203 Norecrin M1 1955 prototype with a 130 kW 180 hp Lycoming O 360 engine derated to 120 kW 160 hp 1204 Norecrin Powered by a 93 kW 125 hp Continental C125 flat four engine 1204 II Norecrin Powered by a 108 kW 145 hp Continental C145 2 flat four engine Operators edit nbsp BrazilOMTA One aircraft only Military operators edit nbsp ArgentinaArgentine Coast Guard nbsp FranceFrench Air Force French Navy nbsp IsraelIsraeli Air Force Two aircraft only operated 1948 1949 1 nbsp SwitzerlandSwiss Air ForceSpecifications 1203 Norecrin II edit nbsp Nord 1200 2 view drawing from L Aerophile March 1946Data from The Illustrated Encyclopedia of Aircraft Part Work 1982 1985 Orbis Publishing p 2616 General characteristicsCrew one Capacity three passengers Length 7 21 m 23 ft 8 in Wingspan 10 22 m 33 ft 6 25 in Height 2 90 m 9 ft 6 in Wing area 13 m2 139 93 sq ft Empty weight 652 kg 1 437 lb Gross weight 1 050 kg 2 315 lb Powerplant 1 Regnier 4L 00 air cooled inverted inline piston engine 101 kW 135 hp Performance Maximum speed 280 km h 174 mph 151 kn Range 900 km 559 mi 486 nmi Service ceiling 5 000 m 16 405 ft References edit Aloni 2005 pp 54 55 nbsp Wikimedia Commons has media related to Nord 1200 Aloni Shlomo September 2005 Ils furent les deux premiers avions francais de l armee israelienne Les deux Norecrin d Israel Le Fana de l Aviation in French No 430 pp 52 55 Cuny Jean 1989 Les avions de combat francais 2 Chasse lourde bombardement assaut exploration French Combat Aircraft 2 Heavy Fighters Bombers Attack Reconnaissance Docavia in French Vol 30 Ed Lariviere OCLC 36836833 Salatin Claude March 2002 Courrier des Lecteurs Readers Letters Avions Toute l Aeronautique et son histoire in French 108 2 ISSN 1243 8650 Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions The Illustrated Encyclopedia of Aircraft Part Work 1982 1985 Orbis Publishing p 2616 Le Trait d Union The Norecrin serie by Claude Salaun issue 109 to 121 1986 1988 French branch of Air Britain nbsp This article on an aircraft of the 1940s is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title Nord Norecrin amp oldid 1165545924, wikipedia, wiki, book, books, library,

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