Kawasaki OH-1 Ninja
Photo ©: Mike Leonard (photos at airliners.net)
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.
| Crew | 2 | |
| Propulsion | 2 Turboshaft Engines | |
| Engine Model | Mitsubishi TS1-10 | |
| Engine Power (each) | 1185 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 | 4 / Fenestron |
| Main Rotor Diameter | 11,60 m | 38,1 ft |
| Rotor Disc Area | 105,7 m² | 1138 ft² |
| Length (Fuselage) | 12,00 m | 39,4 ft |
| Length | 13,40 m | 44,0 ft |
| Height | 3,80 m | 12,5 ft |
| First Flight | 06.08.1996 | |
| Production Status | in production | |
| ICAO Code | OH1 | |
| Data for (Version) | Kawasaki OH-1 Ninja | |
| Extras | |
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