|
|
|
| Prime contractor |
NATO Helicopter Industries |
| Country of
origin |
Italy, France,
Germany and the Netherlands |
| Type |
Tactical
Transport Helicopter / NATO Frigate Helicopter |
| Crew |
1 to 4 |
| First flight |
1995 |
| In-service
year |
Expected in 2007 |
| Engine |
Twin Engine, Rolls-Royce/Turbomeca RTM 322-01/9
or General Electric T700-T6E turboshafts |
| Ceiling |
6000 m |
| Speed |
300 km/h |
| Main
rotor diameter |
16.30
m |
Length, rotors turning
|
19.56 m |
Height, rotors turning
|
5.23 m |
| Weight empty |
5400 kg |
| Max. take-off
weight |
9100 kg |
| Cannon |
|
| Armament |
|
|
|
|
