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At a glance
Measured figures
Fajr F.3 · Length
Single source8.07 m (26 ft 6 in)[source]
KT-1 · Length
Single sourceConfiguration
| Specification | Fajr F.3 | KAI KT-1 Woongbi |
|---|---|---|
| Type | Training aircraft[source] | Basic trainer and light attack aircraft[source] |
| Manufacturer | Fajr Aviation & Composites Industry[source] | Korea Aerospace Industries[source] |
| Status | Active service[source] | In service[source] |
| Primary user | Iranian Air Force[source] | — |
10.3 m (33 ft 10 in)[source]
Fajr F.3 · Range
Single source1,129 km (702 mi, 610 nmi)[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]
Fajr F.3 · 1 × Lycoming AEIO-540-L1B5 6-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-540-L1B5 6-cylinder air-cooled horizontally-opposed piston engine, 201 kW (270 hp)[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured |
|---|
2001—[source] |
1999–present[source] |
| Introduction date | Iran[source] | 2000[source] |
|---|
| First flight | 1995[source] | November 1991[source] |
|---|
| Capacity | 3 pax[source] | — |
|---|
| Airfoil | Horstmann-Quast HQ-42E[source] | root: NACA 63-218 ; tip: NACA 63-212[source] |
|---|
| Fuel capacity | 212 L (56 US gal; 47 imp gal)[source] | 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] |
|---|
| Cabin Width | 1.25 m (4 ft 1 in)[source] | — |
|---|
| Propellers | 3-bladed constant-speed propeller[source] | 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 | 104 km/h (65 mph, 56 kn)[source] | 132 km/h (82 mph, 71 kn) flaps down[source] |
|---|
| Never exceed speed | 370 km/h (230 mph, 200 kn)[source] | 648 km/h (403 mph, 350 kn)[source] |
|---|
| Take-off run | 310 m (1,017 ft)[source] | — |
|---|
| Landing run | 370 m (1,214 ft)[source] | — |
|---|
| National origin | Iran[source] | South Korea[source] |
|---|
| Designer | — | Agency for Defence Development Korea Aerospace Industries[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] |
|---|
| Aspect ratio | — |
|---|
| Maximum fuel weight | — | 408 kg (899 lb)[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] |
|---|
Maximum take-off; KT-1 · (and Maximum Landing Weight)with external stores
Single source