Nord 2100 Norazur
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Nord 2100 Norazur
Le Nord 2100 Norazur sur Wikipedia de langue anglaise :
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The Nord 2100 Norazur was a 1940s French civil transport monoplane designed and built at Courbevoie near Paris by SNCAN.
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The Nord 2100 Norazur was a 1940s French civil transport monoplane designed and built at Courbevoie near Paris by SNCAN.
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Design and development
The Norazur was a high-wing cantilever monoplane with a retractable tricycle landing gear.
Powered by two wing-mounted Potez piston engines in pusher configuration.
It had an enclosed cabin for ten passengers or freight.
Designed to meet a post-war requirement for a light transport and training aircraft the Norazur first flew at Les Moreuax on 30 April 1947.
An additional prototype with 390hp Bearn 6D-07 engines is believed to have been built
With other similar designs available the type did not enter production.
The Norazur was a high-wing cantilever monoplane with a retractable tricycle landing gear.
Powered by two wing-mounted Potez piston engines in pusher configuration.
It had an enclosed cabin for ten passengers or freight.
Designed to meet a post-war requirement for a light transport and training aircraft the Norazur first flew at Les Moreuax on 30 April 1947.
An additional prototype with 390hp Bearn 6D-07 engines is believed to have been built
With other similar designs available the type did not enter production.
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- Messages : 1156
Re: Nord 2100 Norazur
Variants
N2100
Prototype light transport with two 420hp Potez 8D-03 piston engines in pusher configuration, one built.
N2101
Prototype with alternate 390hp Beard 6D-07 engines, believed to have been built.
N2102
Projected variant with two Snecma 125 engines in tractor configuration.
N2100
Prototype light transport with two 420hp Potez 8D-03 piston engines in pusher configuration, one built.
N2101
Prototype with alternate 390hp Beard 6D-07 engines, believed to have been built.
N2102
Projected variant with two Snecma 125 engines in tractor configuration.
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Specifications
General characteristics
* Crew: 2
* Capacity: 10 passengers
* Length: 13.5 m (44 ft 3 in)
* Wingspan: 18.0 m (59 ft 1 in)
* Height: 3.85 m (12 ft 8 in)
* Wing area: 38 m2 (410 sq ft)
* Empty weight: 3,280 kg (7,231 lb)
* Gross weight: 4,630 kg (10,207 lb)
* Powerplant: 2 × Potez 8D-03 piston engines in pusher configuration, 310 kW (420 hp) each
General characteristics
* Crew: 2
* Capacity: 10 passengers
* Length: 13.5 m (44 ft 3 in)
* Wingspan: 18.0 m (59 ft 1 in)
* Height: 3.85 m (12 ft 8 in)
* Wing area: 38 m2 (410 sq ft)
* Empty weight: 3,280 kg (7,231 lb)
* Gross weight: 4,630 kg (10,207 lb)
* Powerplant: 2 × Potez 8D-03 piston engines in pusher configuration, 310 kW (420 hp) each
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Performance
* Maximum speed: 340 km/h (210 mph; 180 kn) at 1500m
* Cruising speed: 312 km/h (194 mph; 168 kn) at 3000m
* Range: 1,100 km (684 mi; 594 nmi)
* Service ceiling: 6,500 m (21,325 ft)
* Maximum speed: 340 km/h (210 mph; 180 kn) at 1500m
* Cruising speed: 312 km/h (194 mph; 168 kn) at 3000m
* Range: 1,100 km (684 mi; 594 nmi)
* Service ceiling: 6,500 m (21,325 ft)
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