North American P-51D Mustang
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- Status:
- Concluído
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21 November 2013, 04:19
Frank Riera
North American P-51D Mustang
'Lollipoop', 10, 1st Lt. Spurgeon Ellington, 100th FS Tuskegee Airmen, US Army Air Force | Natural Metal | WW2, Ramitelli IT (December 1944)
Specifications (P-51D Mustang)
General characteristics
Crew: 1
Length: 32 ft 3 in (9.83 m)
Wingspan: 37 ft 0 in (11.28 m)
Height: 13 ft 4½ in (4.08 m:tail wheel on ground, vertical propeller blade.)
Wing area: 235 sq ft (21.83 m²)
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 × Packard V-1650-7 liquid-cooled supercharged V-12, 1,490 hp
(1,111 kW) at 3,000 rpm;[89] 1,720 hp (1,282 kW) at WEP
Zero-lift drag coefficient: 0.0163
Drag area: 3.80 sqft (0.35 m²)
Aspect ratio: 5.83
Performance
Maximum speed: 437 mph (380 kn, 703 km/h) at 25,000 ft (7,600 m)
Cruise speed: 362 mph (315 kn, 580 km/h)
Stall speed: 100 mph (87 kn, 160 km/h)
Range: 1,650 mi (1,434 nmi, 2,755 km)with external tanks
Service ceiling: 41,900 ft (12,800 m)
Rate of climb: 3,200 ft/min (16.3 m/s)
Wing loading: 39 lb/sqft (192 kg/m²)
Power/mass: 0.18 hp/lb (300 W/kg)
Lift-to-drag ratio: 14.6
Recommended Mach limit 0.8
Armament
6× 0.50 caliber (12.7mm) M2 Browning machine guns with 1,880 total rounds
(400 rounds for each on the inner pair, and 270 rounds for each of the outer
two pair)
2× hardpoints for up to 2,000 lb (907 kg) of bombs
6 or 10× T64 5.0 in (127 mm) H.V.A.R rockets (P-51D-25, P-51K-10 on)[
North American P-51D Mustang
'Lollipoop', 10, 1st Lt. Spurgeon Ellington, 100th FS Tuskegee Airmen, US Army Air Force | Natural Metal | WW2, Ramitelli IT (December 1944)
Specifications (P-51D Mustang)
General characteristics
Crew: 1
Length: 32 ft 3 in (9.83 m)
Wingspan: 37 ft 0 in (11.28 m)
Height: 13 ft 4½ in (4.08 m:tail wheel on ground, vertical propeller blade.)
Wing area: 235 sq ft (21.83 m²)
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 × Packard V-1650-7 liquid-cooled supercharged V-12, 1,490 hp
(1,111 kW) at 3,000 rpm;[89] 1,720 hp (1,282 kW) at WEP
Zero-lift drag coefficient: 0.0163
Drag area: 3.80 sqft (0.35 m²)
Aspect ratio: 5.83
Performance
Maximum speed: 437 mph (380 kn, 703 km/h) at 25,000 ft (7,600 m)
Cruise speed: 362 mph (315 kn, 580 km/h)
Stall speed: 100 mph (87 kn, 160 km/h)
Range: 1,650 mi (1,434 nmi, 2,755 km)with external tanks
Service ceiling: 41,900 ft (12,800 m)
Rate of climb: 3,200 ft/min (16.3 m/s)
Wing loading: 39 lb/sqft (192 kg/m²)
Power/mass: 0.18 hp/lb (300 W/kg)
Lift-to-drag ratio: 14.6
Recommended Mach limit 0.8
Armament
6× 0.50 caliber (12.7mm) M2 Browning machine guns with 1,880 total rounds
(400 rounds for each on the inner pair, and 270 rounds for each of the outer
two pair)
2× hardpoints for up to 2,000 lb (907 kg) of bombs
6 or 10× T64 5.0 in (127 mm) H.V.A.R rockets (P-51D-25, P-51K-10 on)[
24 December 2013, 04:14