To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Nord 2100 Norazur

From Wikipedia, the free encyclopedia

2100 Norazur
Role Ten-passenger transport monoplane
National origin France
Manufacturer Nord Aviation
First flight 30 April 1947
Number built 1

The Nord 2100 Norazur was a 1940s French military transport monoplane designed and built at Courbevoie near Paris by SNCAN.[1][2]

Design and development

The Norazur was a high-wing cantilever monoplane with a retractable tricycle landing gear.[1] Powered by two wing-mounted Potez piston engines in pusher configuration.[1] It had an enclosed cabin for ten passengers or freight.[1]

Designed to meet a post-war requirement for a light transport and training aircraft the Norazur first flew at Les Mureaux on 30 April 1947.[2] An additional prototype with 290 kW (390 hp) Béarn 6D-07 engines is believed to have been built.[2] With other similar designs available the type did not enter production.[2]

Variants

N2100
Prototype light transport with two 310 kW (420 hp) Potez 8D-03 inverted, air-cooled V-8 piston engines in pusher configuration,[3] one built.[2]
N2101
Prototype with alternate 290 kW (390 hp) Béarn 6D-07 inverted, air-cooled V-6 piston engines in pusher configuration,[3] believed to have been built.[2]
N2102
Projected variant with two SNECMA 12S engines in tractor configuration.[2]

Specifications

Data from [2]

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 inverted V-8 piston engines in pusher configuration[3], 310 kW (420 hp) each

Performance

  • Maximum speed: 340 km/h (210 mph, 180 kn) at 1500m
  • Cruise speed: 312 km/h (194 mph, 168 kn) at 3000m
  • Range: 1,100 km (680 mi, 590 nmi)
  • Service ceiling: 6,500 m (21,300 ft)

Notes

  1. ^ a b c d "Un Nouvel Avion Francais". Flight. 29 May 1947. p. 506. ISSN 1368-485X.
  2. ^ a b c d e f g h Chillon et al, 1980, p. 97
  3. ^ a b c Jane's All the World's Aircraft 1950-51, p.150c

Bibliography

  • Bridgman, Leonard (1950). Jane's All the World's Aircraft 1950-51. London: Sampson, Low, Marston and Co. Ltd. p. 150c.
  • Chillon, Jacques; Dubois, Jean-Pierre & Wegg, John (1980). French Post-War Transport Aircraft. Tonbridge, UK: Air-Britain. ISBN 0-85130-078-2.
  • Photo of N-2100
This page was last edited on 26 October 2023, at 16:52
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.