| North American P-51 Mustang |
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| North American P-51 Mustang |
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| Country:
USA |
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Type: Fighter |
| Manufacturer:
North American |
| Service:
1942 - 1957 |
| First
Flight: 26 October 1940 |
| Production:
15875 |
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The North American Aviation P-51 Mustang was an American long-range single-seat fighter aircraft that entered service with Allied air forces in the middle years of World War II.
The P-51 flew most of its wartime missions as a bomber escort in raids over Germany, helping ensure Allied air superiority from early 1944. It also saw limited service against the Japanese in the Pacific War. The Mustang began the Korean War as the United Nations' main fighter, but was relegated to a ground attack role when superseded by jet fighters early in the conflict. Nevertheless, it remained in service with some air forces until the early 1980s.
As well as being economical to produce, the Mustang was a fast, well-made, and highly durable aircraft. The definitive version of the single-seat fighter was powered by the Packard V-1650-3, a two-stage two-speed supercharged 12-cylinder Packard-built version of the legendary Rolls-Royce Merlin engine, and (the P-51D) were armed with six of the aircraft version of the .50 caliber (12.7 mm) Browning machine guns.
After World War II and the Korean conflict, many Mustangs were converted for civilian use, especially air racing. The Mustang fighter had achieved such a reputation that, in the mid-1960s, Ford Designer John Najjar proposed the name for a new youth-oriented coupe after the fighter.
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| TECHNICAL
SPECIFICATIONS ( P-51D Mustang) |
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General characteristics
- Crew: 1
- Length: 32 ft 3 in (9.83 m)
- Wingspan: 37 ft 0 in (11.28 m)
- Height: 13 ft 8 in (4.17 m)
- Wing area: 235 ft (21.83 m)
- Empty weight: 7,635 lb (3,465 kg)
- Loaded weight: 9,200 lb (4,175 kg)
- Max takeoff weight: 12,100 lb (5,490 kg)
- Powerplant: 1 x Packard Merlin V-1650-7 liquid-cooled supercharged V-12, 1,695 hp (1,265 kW)
- Zero-lift drag coefficient: 0.0163
- Drag area: 3.80 ft (0.35 m)
- Aspect ratio: 5.83
Performance
- Maximum speed: 437 mph (703 km/h) at 25,000 ft (7,620 m)
- Cruise speed: 362 mph (580 km/h)
- Stall speed: 100 mph (160 km/h)
- Range: 1,650 mi (2,755 km) with external tanks
- Service ceiling 41,900 ft (12,770 m)
- Rate of climb: 3,200 ft/min (16.3 m/s)
- Wing loading: 39 lb/ft (192 kg/m)
- Power/mass: 0.18 hp/lb (300 W/kg)
- Lift-to-drag ratio: 14.6
- Recommended Mach limit 0.8
Armament
- 6 x 0.50 in (12.7 mm) machine guns; 400 rounds per gun for the two inboard guns; 270 per outboard gun
- 2 hardpoints for up to 2,000 lb (907 kg)
- 10 x 5 in (127 mm) rockets
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