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General Info

Nord-Aviation SA
Nord 2501 Noratlas



A French Air Force Nord Noratlas in flight
Role Military Transport
National origin France
Manufacturer Nord Aviation
First flight 10 September 1949
Introduction 6 December 1953
Retired 1989 (France)
Status Retired
Primary users France
Germany
Greece
Israel
Produced 1949-1961
Number built 425
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History Nord-Aviation SA
Nord 2501 Noratlas

Development commenced during the late 1940s with the aim of producing a suitable aircraft to replace the numerous older types that were in service with the Armée de l'Air (French Air Force) which dated back to the Second World War. In response to a competition organised by the Direction Technique Industrielle (DTI), Nord produced their Nord 2500 proposal, which was selected as the most promising. Experiences with the first prototype, powered by Gnome-Rhône 14R engines, did not impress, thus the design was revised as the Nord 2501, powered by the SNECMA-built Bristol Hercules 738/9 engines instead, which was found acceptable. Accordingly, the Noratlas was introduced to service by the Armée de l'Air on 6 December 1953

The Nord Noratlas was a dedicated military transport aircraft, developed and manufactured by French aircraft manufacturer Nord Aviation.

Design

Nord Aviation N 2501D Noratlas at the Technik Museum, Speyer, Germany

The Nord Noratlas was a purpose-built twin-engine, twin-boom transport aircraft. It featured a large pod-like fuselage that was slung in between the aircraft's twin booms and indirectly attached to them via its shoulder-mounted wing.[1] The Noratlas was deliberately designed to be operated under austere conditions, featuring widely spaced landing gear, complete with wide low-pressure tyres, for additional stability and suitability to moving over rough terrain, while the propellers had sufficient clearance to accommodate such operations as well. It was powered by a pair of SNECMA-built Bristol Hercules 738/9 engines, each of which being capable of producing 2,040 hp (1,520 kW) and driving a four-bladed Rotol propeller

The sizable cabin of the Noratlas was capable of accommodating up to 7.5 short tons (6.8 t) of freight or a maximum of 40 passengers; when flown at a cruising speed of 200 mph (320 km/h), it could transport a 6-ton payload over a range of up to 750 miles (1,210 km). Cargo was typically loaded into and unloaded from the main cabin via the rear-facing clamshell doors, which were intentionally positioned close to ground level to ease freight handling

Civilian N-2502 of Aeromaritime with wingtip Turbomeca Marbore auxiliary jets in 1957
Former Portuguese Air Force N-2502F
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Avions Marcel Dassault-Breguet Aviation

Dassault Aviation SA Avions
Nord-Aviation SA Nord 2501 Noratlas

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General Info

    • Crew: 4-5
    • Capacity: 45 soldiers, 36 paratroopers, 18 patients with medics, or 8,458 kg (18,647 lb) cargo
    • Length: 21.962 m (72 ft 1 in)
    • Wingspan: 32.5 m (106 ft 8 in)
    • Height: 6 m (19 ft 8 in)
    • Wing area: 101.2 m2 (1,089 sq ft)
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Powerplant

  • Empty weight: 13,075 kg (28,825 lb)
  • Max takeoff weight: 20,603 kg
  • Fuel capacity: 5,090 L
  • Powerplant: 2 × SNECMA-manufactured Bristol Hercules 738 14-cylinder air-cooled sleeve-valve radial piston engines, 1,558 kW (2,089 hp) each
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Specifications

  • Maximum speed: 440 km/h (270 mph, 240 kn) at 21,000 kg (46,297 lb) AUW
  • 405 km/h  fully loaded
    • Cruise speed: 324 km/h (201 mph, 175 kn) at 1,500 m (4,900 ft)
    335 km/h (208 mph;  at 3,000 m
    • Range: 2,500 km (1,600 mi, 
    • Service ceiling: 7,500 m 
Special Links Avions Marcel Dassault-Breguet Aviation

Links to Youtube & Others

The Noratlas had been able to attain particular recognition and notoriety amongst the general public as a consequence of its use during the Suez Crisis of 1956.

Nord-Aviation SA
Nord 2501 Noratlas

During its service life with the Armée de l'Air, the Noratlas  operated in it cargo-carrying role;

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Youtube Link

On occasion of the Hamburg Airport Days 2015 the world's last flying Noratlas paid a visit to the airport from 21st August to 23rd August 2015.

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