| KAI KUH-1 Surion
|
| Developer | Korea Aerospace Industry
|
| manufacturer | Korea Aerospace Industry
|
| First flight | March 10, 2010
|
| Production period | 2010 ~ present
|
| Number of production units | More than 276 units expected to be produced
|
| Actual deployment | May 22, 2013 ~ Present
|
| Fuselage | 14.96 m
|
| With rotor | 19.016 m
|
| full width Fuselage | 2.36 m With
|
| rotor | 14.96 m
|
| Full height | 4.5 m
|
| Empty weight | 5,136 kg
|
| Loading weight | 3,572 kg
|
| Fuel loading | 1,159 kg
|
| Takeoff weight | 8,709 kg
|
| Rotor system | Main rotor 4 blades, tail rotor 4 blades
|
| engine | Hanwha Techwin General Electric T700/701K turboshaft engine x 2 units
|
| Engine power | GE T700/701K 1,915 HP x 2 (3,830 HP)
|
| Cruising speed | 251 km/h
|
| Maximum speed | 279 km/h
|
| Range | 450 km
|
| Maximum cruising distance | 775 km
|
| Maximum cruising time | 2 hours 18 minutes
|
| Rate of rise | 8.5 m/s
|
| cruising flight altitude | 3,048 m
|
| Practical ascent limit | 4,590 m
|
| crew | 2 pilots + 2 gunners
|
| passengers | 9 fully armed troops, 11 fully armed troops when relocating seats # (Army type)
|
| Armed | K-12 7.62mm machine gun x 2 doors
|
