Nord Noratlas

· Nord Aviation

Airplanes

Length

21.962 m

Flat Wing Span

32.5 m

Height

6 m

Flat Wing Area

101.2 m²

Flat Wing Aspect Ratio

10.5

Max Seating

Cruise Speed

324 km/h

Max Speed

440 km/h

Max Ceiling

7500 m

Number of Engines

First Flight

1949-09-10

Entry Into service

1953-12-06

Number Built

425

Maximum Take-Off Weight

20.603 t (paragliders: kg)

Total Fuel Capacity

5090

Maximum Range

2500 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Nord Noratlas	20.603	5090	2500

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Vickers Warwick		21.9456	29.2608		Compare
Henschel Hs 130		22	33.01		Compare
Hawker Siddeley HS 748		20.4216	31.0896	58	Compare
Convair C-131 Samaritan		24.14	32.11	48	Compare
Martin 4-0-4	Pratt & Whitney R-2800 Double Wasp	22.5552	28.3464	40	Compare
Ilyushin Il-14		22.3	31.7	32	Compare

All data (30 fields)

Name: Nord Noratlas
Manufacturer: Nord Aviation
Description: The Nord Noratlas is a dedicated military transport aircraft, developed and manufactured by French aircraft manufacturer Nord Aviation.
ICAO Code: NORA
First Flight: 1949-09-10
Entry Into service: 1953-12-06
Production End: 1961-01-01
Service End: 1989-01-01
Designer: Nord Aviation
Type: Military Transport
Length (m): 21.962
Height (m): 6
Cockpit Crew: 4
Max Seating: 36
Max Speed (km/h): 440
Cruise Speed (km/h): 324
Max Ceiling (m): 7500
Rate of Climb (m/s): 6.25
Capacity Description: 45 soldiers, 36 paratroopers, 18 patients with medics, or 8458 kg cargo
National Origin: France
Number Built: 425
Powerplant Description: 2 × SNECMA-manufactured Bristol Hercules 738 14-cylinder air-cooled sleeve-valve radial piston engines, 1558 kW (2089 hp) each
Primary Users: France, Germany , Greece , Israel
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Nord_Noratlas
Flat Wing Span (m): 32.5
Flat Wing Area (m²): 101.2
Flat Wing Aspect Ratio: 10.5
Wake Category: M
Number of Engines: 2