Specifications .28An-124-100M-150.29 Antonov An-124 Ruslan

container being lifted belly of an-124 using on-board overhead crane

data antonov

general characteristics

crew: 4–6 (pilot, copilot, navigator, senior flight engineer (+flight engineer, radio man) + 2 loadmasters)
capacity: 88 passengers or hold can take additional 350 on palletised seating system
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)
useful load: 230,000 kg (508,000 lb)
loaded weight: 405,000 kg (893,000 lb)
max. takeoff weight: 405,000 kg (893,000 lb)
powerplant: 4 × 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: 5,200 km (2,808 nm, 3231 mi)
service ceiling: 12,000 m (39,370 ft)
wing loading: 645 kg/m² (74.7 lb/sq ft)
thrust/weight: 0.23
take-off run distance (maximum take-off weight): 2,520 m (8,270 ft)
landing roll distance @ maximum landing weight: 900 m (3,000 ft)

flight range

an-124-100


0 tons of cargo= 15,000 km (8,100 nmi)
10 tons of cargo= 14,100 km (7,613 nmi)
20 tons of cargo= 13,250 km (7,154 nmi)
30 tons of cargo= 12,300 km (6,641 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= 7,100 km (3,834 nmi)
97 tons of cargo= 6,500 km (3,510 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)


Аn-124-100М-150


40 tons of cargo= 11,900 km (6,425 nmi)
92 tons of cargo= 7,500 km (4,050 nmi)
113 tons of cargo= 5,900 km (3,186 nmi)
120 tons of cargo= 5,400 km (2,916 nmi)
122 tons of cargo= 5,200 km (2,808 nmi)
150 tons of cargo= 3,200 km (1,728 nmi)




^ an-124-100 performance . antonov. retrieved 10 august 2013. 
^ an-124 virtual loading @ volga-dnepr . archived original on 30 april 2008.