.jpg "Nord 2501D (2508 Noratlas) Transport aircraft. First flight: 1949 © Konstantinos Panitsidis")
In numbers Through the lens Video
Technical specifications
|
DESIGNER
|
Nord |
|---|---|
|
COUNTRY
|
France |
|
TYPE
|
Transport aircraft |
|
CREW
|
4 - 5 |
|
POWER-PLANT
|
Two SNECMA Bristol Hercules 739 piston engine |
|
Power, h.p.
|
2x2.040
|
|
DIMENSIONS
|
|
|
Length, m
|
21,95
|
|
Height, m
|
6,00 |
|
Wing span, m
|
32,50
|
|
Wing area m2
|
101,20
|
| WEIGHT | |
| Maximum take-off, kg | 21.000 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 13.075 |
| Internal fuel, kg | - |
| Payload, kg | |
| - freight in cabin | 6.800 (7.880) |
| - soldiers | up to 45 |
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
440 |
|
Cruising speed, km/h
|
396 |
|
Maximum overload, g
|
-
|
|
Rate of climb, m/min
|
-
|
| Service ceiling, m | 7.500 |
|
Ferry range, km
|
- |
|
Range, km
|
3.000
|
| Combat range, km | - |
| ARMAMENT | Doesn't have (defensive). |
Photos Nord 2501D/2508 Noratlas
