Overview
The Lockheed P-38 Lightning stood out from every other fighter of its era with its distinctive twin-boom design and central cockpit nacelle. Developed before World War II, it became one of the United States’ most versatile combat aircraft, serving as a fighter, interceptor, reconnaissance platform, and ground-attack aircraft across multiple theaters.
Specifications
Units
- Engine
- 2 × Allison V-1710-111/113
- Engine type
- Piston
- Power
- 2 × 1,600 hp · 1,193 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 1
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 37 ft 10 in · 11.53 m
- Tail height
- 12 ft 10 in · 3.90 m
- Fuselage diameter
- 3 ft 3 in · 1.00 m
- Wing span
- 52 ft 0 in · 15.85 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 21,600 lb · 9,800 kg
- Max landing weight
- 17,500 lb · 7,950 kg
- Max payload
- 3,950 lb · 1,800 kg
- Fuel capacity
- 1,160 gal · 4,400 L · 3,200 kg (AvGas)
- Max cruise speed
- 360 kt · 414 mph · 667 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 91 kt · 105 mph · 169 km/h
- Range
- 1,995 nm · 2,300 mi · 3,690 km
- Fuel burn
- —
- Ceiling
- 44,000 ft · 13,400 m
- Rate of climb
- 4,750 ft/min · 24 m/s
- Takeoff distance
- 2,200 ft · 670 m
- Landing distance
- 2,300 ft · 700 m
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