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MilborneOne · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Cessna 152 · Length
Single source24 ft 1 in (7.34 m)[source]
KT-1 · Length
Single sourceConfiguration
| Specification | Cessna 152 | KAI KT-1 Woongbi |
|---|---|---|
| Type | Basic trainer , GA private aircraft[source] | Basic trainer and light attack aircraft[source] |
| National origin | United States[source] | South Korea[source] |
| Manufacturer | Cessna[source] | Korea Aerospace Industries[source] |
| Primary users | Mexican Navy Bangladesh Army Bolivian Air Force[source] |
10.3 m (33 ft 10 in)[source]
Cessna 152 · Range
Single sourceFerry; Cessna 152 · with long-range tanks
Single source477 mi (768 km, 415 nmi)[source]
795 mi (1,279 km, 691 nmi) with long-range tanks[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 sourceKT-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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Republic of Korea Air Force Indonesian Air Force Turkish Air Force Peruvian Air Force Senegalese Air Force[source]
| Number built | 7,584[source] | 186[source] |
|---|
| Manufactured | 1977–1985[source] | 1999–present[source] |
|---|
| Introduction date | 1977[source] | 2000[source] |
|---|
| Developed from | Cessna 150[source] | — |
|---|
| Capacity | one passenger (plus two children not exceeding 120 lb (54 kg) on optional baggage compartment bench seat)[source] | — |
|---|
| Propellers | 2-bladed fixed pitch, 69 inches (175 cm) McCauley or 72 in (183 cm) Sensenich 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 | 49 mph (79 km/h, 43 kn) (power off, flaps down)[source] | 132 km/h (82 mph, 71 kn) flaps down[source] |
|---|
| Designer | — | Agency for Defence Development Korea Aerospace Industries[source] |
|---|
| Status | — | In service[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] |
|---|
| 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] |
|---|
Maximum take-off; KT-1 · (and Maximum Landing Weight)with external stores
Single source