| Manufacturer |
McDonnell Douglas |
Antonov |
| Description |
The McDonnell Douglas MD-12 was a large wide-body airliner concept planned by McDonnell Douglas in the 1990s. |
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 |
McDonnell Douglas |
Antonov |
| Type |
Double-decker wide-body aircraft |
Heavy transport aircraft |
| Length (m) |
63.4 |
69.1 |
| Height (m) |
22.55 |
21.08 |
| Cockpit Crew |
2 |
|
| Max Seating |
430 |
88 |
| Max Speed (km/h) |
1050 |
|
| Cruise Speed (km/h) |
|
865 |
| Max Ceiling (m) |
|
12000 |
| Capacity Description |
Long range: 430 passengers (3-class) / High-capacity: 511 passengers (1-class) |
88 passengers in upper aft fuselage, or the hold can take an additional 350 pax on a palletised seating system / 120000 kg |
| Max Mach (Mach) |
0.85 |
|
| National Origin |
United States of America |
Soviet Union |
| Number Built |
|
57 |
| Powerplant Description |
4 × General Electric CF6-80C2 high-bypass turbofans, 274 kN thrust each |
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 |
Design study, cancelled |
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/McDonnell_Douglas_MD-12 |
en.wikipedia.org/wiki/Antonov_An-124_Ruslan |
| Flat Wing Span (m) |
64.92 |
73.3 |
| Flat Wing Area (m²) |
543.1 |
628 |
| Flat Wing Aspect Ratio |
|
8.6 |
| Wake Category |
|
H |
| Aircraft Engine |
General Electric CF6 |
Progress D-18T |
| Number of Engines |
4 |
4 |