Antonov An-124 Ruslan: Difference between revisions
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[[Category:Cargo Transporters]] | [[Category:Cargo Transporters]] | ||
Data from antonov.com[25] | |||
General characteristics | |||
* Crew: 6 | |||
* Capacity: 88 passengers | |||
* Payload: 150,000 kg (330,000 lb) | |||
* Length: 68.96 m (226 ft 3 in) | |||
* Wingspan: 73.3 m (240 ft 5 in) | |||
* Height: 20.78 m (68 ft 2 in) | |||
* Wing area: 628 m² (6,760 sq ft) | |||
* Empty weight: 175,000 kg (385,000 lb) | |||
* Loaded weight: 405,000 kg (892,000 lb) | |||
* Useful load: 230,000 kg (508,000 lb) | |||
* Max takeoff weight: 405,000 kg (893,000 lb) | |||
* Powerplant: 4× Ivchenko Progress D-18T turbofans, 229.5 kN (51,600 lbf) each | |||
Performance | |||
* Maximum speed: 865 km/h (467 kn (537 mph)) | |||
* Cruise speed: 800-850 km/h (430 kn (490 mph)) | |||
* Range: 5,400 km (2,900 nm, 3,360 mi (5,410 km)) | |||
* Service ceiling: 12,000 m (35,000 ft) | |||
* Wing loading: 365 kg/m² (74.7 lb/sq ft) | |||
* Thrust/weight: 0.41 | |||
[edit] Flight range | |||
An-124-100 | |||
* 0 tons of cargo = 15,000 km (8,100 nmi) [26] | |||
* 10 tons of cargo = 14,125 km (7,627 nmi) | |||
* 20 tons of cargo = 13,250 km (7,154 nmi) | |||
* 30 tons of cargo = 12,375 km (6,682 nmi) | |||
* 40 tons of cargo = 11,500 km (6,210 nmi) | |||
* 72 tons of cargo = 8,700 km (4,698 nmi) | |||
* 90 tons of cargo = 7,125 km (3,847 nmi) | |||
* 97 tons of cargo = 6,495 km (3,507 nmi) | |||
* 104 tons of cargo = 5,900 km (3,186 nmi) | |||
* 108 tons of cargo = 5,550 km (2,997 nmi) | |||
* 120 tons of cargo = 4,500 km (2,430 nmi) | |||
* 122 tons of cargo = 4,325 km (2,335 nmi) | |||
Аn-124-100М-150 | |||
* 92 tons of cargo = 7,500 km (4,050 nmi) | |||
* 113 tons of cargo = 5,925 km (3,199 nmi) | |||
* 120 tons of cargo = 5,400 km (2,916 nmi) | |||
* 122 tons of cargo = 5,250 km (2,835 nmi) |
Revision as of 22:53, 15 September 2009
Antonov An-124 Ruslan at a Glance | |
---|---|
Role | Cargo Transport |
Country of Origin | Russia and Ukrain |
Manufacturer | Antonov |
Status | In production |
Number Built | 56 |
Unit Cost | US$50-80 million |
File:Airplanes-Antonov An-124 Ruslan.jpg |
Data from antonov.com[25]
General characteristics
* Crew: 6 * Capacity: 88 passengers * Payload: 150,000 kg (330,000 lb) * Length: 68.96 m (226 ft 3 in) * Wingspan: 73.3 m (240 ft 5 in) * Height: 20.78 m (68 ft 2 in) * Wing area: 628 m² (6,760 sq ft) * Empty weight: 175,000 kg (385,000 lb) * Loaded weight: 405,000 kg (892,000 lb) * Useful load: 230,000 kg (508,000 lb) * Max takeoff weight: 405,000 kg (893,000 lb) * Powerplant: 4× Ivchenko Progress D-18T turbofans, 229.5 kN (51,600 lbf) each
Performance
* Maximum speed: 865 km/h (467 kn (537 mph)) * Cruise speed: 800-850 km/h (430 kn (490 mph)) * Range: 5,400 km (2,900 nm, 3,360 mi (5,410 km)) * Service ceiling: 12,000 m (35,000 ft) * Wing loading: 365 kg/m² (74.7 lb/sq ft) * Thrust/weight: 0.41
[edit] Flight range
An-124-100
* 0 tons of cargo = 15,000 km (8,100 nmi) [26] * 10 tons of cargo = 14,125 km (7,627 nmi) * 20 tons of cargo = 13,250 km (7,154 nmi) * 30 tons of cargo = 12,375 km (6,682 nmi) * 40 tons of cargo = 11,500 km (6,210 nmi) * 72 tons of cargo = 8,700 km (4,698 nmi) * 90 tons of cargo = 7,125 km (3,847 nmi) * 97 tons of cargo = 6,495 km (3,507 nmi) * 104 tons of cargo = 5,900 km (3,186 nmi) * 108 tons of cargo = 5,550 km (2,997 nmi) * 120 tons of cargo = 4,500 km (2,430 nmi) * 122 tons of cargo = 4,325 km (2,335 nmi)
Аn-124-100М-150
* 92 tons of cargo = 7,500 km (4,050 nmi) * 113 tons of cargo = 5,925 km (3,199 nmi) * 120 tons of cargo = 5,400 km (2,916 nmi) * 122 tons of cargo = 5,250 km (2,835 nmi)