Attribute | Antonov An-124 Ruslan × | Rockwell B-1B Lancer × |
---|---|---|
General | ||
Manufacturer | Antonov | Rockwell International |
Model | Antonov An-124 Ruslan | Rockwell B-1B Lancer |
Country | Ukraine | United States |
Manufactured from (year) | 1986 | 1983 |
Manufactured to (year) | 2004 | 1988 |
Type | Cargo Airplanes | Military Aircraft |
Icao | A124 | B1 |
Performance | ||
Engine | 4x 4 × Ivchenko Progress D-18T turbofans | 4x 4 × General Electric F101-GE-102 |
Power, lbf (lbf) | 51,600 | 30,780 |
Avionics | - | AN/APQ-164, AN/ALQ-161, AN/ASQ-184 |
Max cruise speed (km/h) | 865 | 1,528 |
Approach speed (km/h) | 259 | 463 |
Travel range (km) | 16,483 | 12,010 |
Fuel economy (km/l) | 0.044 | 0.078 |
Service ceiling (m) | 11,887 | 18,288 |
Rate of climb (m/sec) | 6.6 | 30.48 |
Take off distance (m) | 3,000 | 600 |
Landing distance (m) | 900 | 420 |
Weights | ||
Max take off weight (kg) | 405,000 | 216,634 |
Max payload (kg) | 136,078 | 34,019 |
Fuel tank capacity (l) | 348,749 | 149,875 |
Baggage volume (m³) | 33 | - |
Dimensions | ||
Seats | 88 | 4 |
Cabin height (m) | 4.4 | - |
Cabin width (m) | 6.4 | - |
Cabin length (m) | 36 | - |
Exterior length (m) | 69.1 | 44.8 |
Tail height (m) | 21.08 | 10.4 |
Fuselage diameter (m) | 4.7 | 2.6 |
Wing span (m) | 73.3 | 41.8 |
Wing tips | No Winglets | No Winglets |