The Lockheed P-38 Lightning was a World War II American fighter aircraft built
by Lockheed. Developed to a United States Army Air Corps requirement, the
P-38 had distinctive twin booms and a single, central nacelle containing the
cockpit and armament.
Maximum speed: xx443 mph (713 km/h) (712 km/h) on War Emergency Power:
1,725 hp at 64 inHG and 28,000 ft (8,530 m)
Stall speed: xx105 mph (169 km/h) (170 km/h)
Range: xx1,300 mi (2,100 km) combat (1,770 km / 3,640 km)
Service ceiling: xx44,000 ft (13,000 m) (13,400 m)
Rate of climb: 4,750 ft/min (24.1 m/s) maximum
Wing loading: 53.4 lb/ft²[94] (260.9 kg/m²)
Power/mass: 0.16 hp/lb (0.27 kW/kg)
Lift-to-drag ratio: 13.5
by Lockheed. Developed to a United States Army Air Corps requirement, the
P-38 had distinctive twin booms and a single, central nacelle containing the
cockpit and armament.
Maximum speed: xx443 mph (713 km/h) (712 km/h) on War Emergency Power:
1,725 hp at 64 inHG and 28,000 ft (8,530 m)
Stall speed: xx105 mph (169 km/h) (170 km/h)
Range: xx1,300 mi (2,100 km) combat (1,770 km / 3,640 km)
Service ceiling: xx44,000 ft (13,000 m) (13,400 m)
Rate of climb: 4,750 ft/min (24.1 m/s) maximum
Wing loading: 53.4 lb/ft²[94] (260.9 kg/m²)
Power/mass: 0.16 hp/lb (0.27 kW/kg)
Lift-to-drag ratio: 13.5
| Lockheed P-38 Lightning Micro Paper Airplane |
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