FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
Measured figures
KT-1 · Length
Single source10.3 m (33 ft 10 in)[source]
Configuration
| Specification | IRIAF Parastu-14 | KAI KT-1 Woongbi |
|---|---|---|
| Type | Trainer aircraft[source] | Basic trainer and light attack aircraft[source] |
| Manufacturer | HESA[source] | Korea Aerospace Industries[source] |
| Designer | Islamic Republic of Iran Air Force[source] | Agency for Defence Development Korea Aerospace Industries[source] |
| Status | Active service[source] | In service |
KT-1 · Wingspan
Single source10.6 m (34 ft 9 in)[source]
KT-1 · Height
Single source3.7 m (12 ft 2 in)[source]
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]
Maximum; KT-1 · at 4,570 m (14,993 ft)
Single source644 km/h (400 mph, 348 kn) at 4,570 m (14,993 ft)[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]
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]
KT-1 · Wing area
Single source16.01 m 2 (172.3 sq ft)[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 · Service ceiling
Single source11,580 m (37,990 ft)[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.
| Primary user | Islamic Republic of Iran Air Force[source] | — |
|---|
| Introduction date | September 2013 (Unveiled)[source] | 2000[source] |
|---|
| Developed from | Beechcraft 33 Bonanza[source] | — |
|---|
| National origin | Iran[source] | South Korea[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] |
|---|
| Manufactured | — | 1999–present[source] |
|---|
| First flight | — | November 1991[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] |
|---|
| 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] |
|---|
| Stall speed | — | 132 km/h (82 mph, 71 kn) flaps down[source] |
|---|
| Never exceed speed | — | 648 km/h (403 mph, 350 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] |
|---|
| Power/mass | — | 0.2137 kW/kg (0.1300 hp/lb)with external stores[source] |
|---|