Lockheed P-38 Lightning

Specifications (P-38L)
General characteristics
Crew: One
Length: 37 ft 10 in (11.53 m)
Wingspan: 52 ft 0 in (15.85 m)
Height: 12 ft 10 in (3.91 m)
Wing area: 327.5 ft² (30.43 m²)
Airfoil: NACA 23016 / NACA 4412
Empty weight: 12,800 lb (5,800 kg)
Loaded weight: 17,500 lb (7,940 kg)
Max takeoff weight: 21,600 lb (9,798 kg)
Powerplant: 2× Allison V-1710-111/113 V-12 piston engine, 1,725 hp (1,194 kW) each Zero-lift drag coefficient: 0.0268
Drag area: 8.78 ft² (0.82 m²)
Aspect ratio: 8.26
Performance
Maximum speed: 443 mph (712 km/h) on War Emergency
Power: 1,725 hp at 64 inHG and 28,000 ft (8530 m)
Stall speed: 105 mph (170 km/h) Range: 1,300 mi combat (1,770 km / 3,640 km)
Service ceiling: 44,000 ft (13,400 m)
Rate of climb: 4,750 ft/min (1,448 m/min)
maximum Wing loading: 53.4 lb/ft² (260.9 kg/m²)
Power/mass: 0.16 hp/lb (0.27 kW/kg) Lift-to-drag ratio: 13.5