Flat Wing Aspect Ratio
8.6
Entry Into service
1986-01-01
Maximum Take-Off Weight
402 t (paragliders: kg)
Total Fuel Capacity
262715.2
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Antonov An-124 Ruslan |
402 |
262715.2 |
3700 |
Similar airplanes
All data (27 fields)
- Name
- Antonov An-124 Ruslan
- Manufacturer
- Antonov
- Description
- The Antonov An-124 Ruslan (; ; NATO reporting name: Condor) is a large, strategic airlift, four-engined aircraft that was designed in the 1980s by the Antonov Design Bureau in the Ukrainian SSR of the Soviet Union (USSR).
- ICAO Code
- A124
- First Flight
- 1982-12-24
- Entry Into service
- 1986-01-01
- Production End
- 2004-01-01
- Designer
- Antonov
- Type
- Heavy transport aircraft
- Length (m)
- 69.1
- Height (m)
- 21.08
- Max Seating
- 88
- Cruise Speed (km/h)
- 865
- Max Ceiling (m)
- 12000
- Capacity Description
- 88 passengers in upper aft fuselage, or the hold can take an additional 350 pax on a palletised seating system / 120000 kg
- National Origin
- Soviet Union
- Number Built
- 57
- Powerplant Description
- 4 × Progress D-18T (D-18 Series 4 on -150 models) high-bypass turbofan engines, 226.8 kN thrust each
- Primary Users
- Russian Aerospace Forces, Volga-Dnepr Airlines , Antonov Airlines , Maximus Air
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Antonov_An-124_Ruslan
- Flat Wing Span (m)
- 73.3
- Flat Wing Area (m²)
- 628
- Flat Wing Aspect Ratio
- 8.6
- Wake Category
- H
- Aircraft Engine
- Progress D-18T
- Number of Engines
- 4