Kawasaki OH-1 Ninja
Observation Helicopter
The Kawasaki OH-1 Ninja is a twin-engined two-seat light observation helicopter produced by the Japanese manufacturer Kawasaki Heavy Industries, operated by the Japan Ground Self-Defense Force.
Propulsion | 2 Turboshaft Engines |
Engine Model | Mitsubishi TS1-10 |
Engine Power (each) | 1186 kW | 1590 shp |
Speed | 306 km/h | 165 kts 190 mph |
Service Ceiling | 4.877 m | 16.000 ft |
Range | 550 km | 297 NM 342 mi. |
Empty Weight | 2.450 kg | 5.401 lbs |
max. Takeoff Weight | 4.000 kg | 8.818 lbs |
Rotor Blades (main/tail) | 4 / Fenestron |
Main Rotor Diameter | 11,60 m | 38 ft 1 in |
Rotor Disc Area | 105,7 m² | 1138 ft² |
Length (Fuselage) | 12,00 m | 39 ft 4 in |
Length | 13,40 m | 43 ft 12 in |
Height | 3,80 m | 12 ft 6 in |
First Flight | 06.08.1996 |
Production Status | in production |
ICAO Code | OH1 |
Data for (Version) | Kawasaki OH-1 Ninja |