Credit
Doo Ho Kim · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Empty; KT-1 · Empty weight
Single sourceGross; KT-1 · Gross weight
Single sourceMaximum take-off; KT-1 · (and Maximum Landing Weight)with external stores
Single source1,910 kg (4,211 lb)[source]
2,540 kg (5,600 lb)[source]
3,311 kg (7,300 lb) (and Maximum Landing Weight)with external stores[source]
Ferry; KT-1 · at 6,100 m (20,013 ft) with max internal and external fuel (30 minutes reserve)
Single sourceKT-1 · at 7,620 m (25,000 ft) with max internal fuel (30 minutes reserve)
Single source1,333 km (828 mi, 720 nmi) at 7,620 m (25,000 ft) with max internal fuel (30 minutes reserve)[source]
2,070 km (1,290 mi, 1,120 nmi) at 6,100 m (20,013 ft) with max internal and external fuel (30 minutes reserve)[source]
Range
Single source579 km (360 mi, 313 nmi)[source]
KT-1 · 1 × Pratt & Whitney Canada PT6A-62 turboprop engine
Single source1 × Pratt & Whitney Canada PT6A-62 turboprop engine, 708.4 kW (950.0 hp)[source]
1 × Salmson 9AB 9-cylinder air-cooled radial piston engine
Single source1 × Salmson 9AB 9-cylinder air-cooled radial piston engine, 170 kW (230 hp)[source]
KT-1 · < at 6,100 m (20,013 ft) with max internal fuel (
Single sourceKT-1 · reserve
Single source<4 hours at 6,100 m (20,013 ft) with max internal fuel (30 minutes reserve)[source]
KT-1 · (3,500 ft/min) at sea level, clean
Single source17.78 m/s (3,500 ft/min) at sea level, clean[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | KAI KT-1 Woongbi | Morane-Saulnier MS.230 |
|---|---|---|
| Type | Basic trainer and light attack aircraft[source] | Elementary Trainer[source] |
| National origin | South Korea[source] | — |
| Manufacturer | Korea Aerospace Industries[source] | Morane-Saulnier[source] |
| Designer | Agency for Defence Development Korea Aerospace Industries[source] | — |
| Status | In service[source] | — |
| Primary users | Republic of Korea Air Force Indonesian Air Force Turkish Air Force Peruvian Air Force Senegalese Air Force[source] | — |
| Number built | 186[source] | 1000+[source] |
| Manufactured | 1999–present[source] | — |
| Introduction date | 2000[source] | — |
| First flight | November 1991[source] | February 1929[source] |
| Fuel capacity | 551 L (146 US gal; 121 imp gal) in two wing tanks with provision for two 189 L (50 US gal; 42 imp gal) drop-tanks on the inboard pylons[source] | 220 L (58 US gal; 48 imp gal) jettison-able fuselage tank with a 22 L (5.8 US gal; 4.8 imp gal) centre-section gravity tank[source] |
| Aspect ratio | — | |
| Airfoil | root: NACA 63-218 ; tip: NACA 63-212[source] | — |
| Maximum fuel weight | 408 kg (899 lb)[source] | — |
| Propellers | 4-bladed Hartzell HC-E4N-2/E9512CB-1, 2.44 m (8 ft 0 in) diameter constant-speed fully feathering reversible propeller[source] | 2-bladed fixed-pitch wooden propeller[source] |
| Stall speed | 132 km/h (82 mph, 71 kn) flaps down[source] | — |
| Never exceed speed | 648 km/h (403 mph, 350 kn)[source] | 260 km/h (160 mph, 140 kn)[source] |
| g limits | + 7 - 3.5 (aerobatic, clean)[source] | — |
| Wing loading | 206.8 kg/m 2 (42.4 lb/sq ft) with external stores[source] | 61.3 kg/m 2 (12.6 lb/sq ft)[source] |
| Power/mass | 0.2137 kW/kg (0.1300 hp/lb)with external stores[source] | 0.1429 kW/kg (0.0869 hp/lb)[source] |
| Primary user | — | Armée de l'Air Flight School, Reims, France[source] |
| Time to altitude | — | 3,000 m (9,800 ft) in 11 minutes 18 seconds[source] |