Comparison of Ilyushin Il-96 300 and Rockwell B-1B Lancer [S]ave
| Attribute |  Ilyushin Il-96 300 × |  Rockwell B-1B Lancer × |
|---|---|---|
| General | ||
| Manufacturer | Ilyushin | Rockwell International |
| Model | Ilyushin Il-96 300 | Rockwell B-1B Lancer |
| Country | Russia | United States |
| Manufactured from (year) | 1992 | 1983 |
| Manufactured to (year) | - | 1988 |
| Type | Jumbo Passenger Jets | Military Aircraft |
| Icao | IL96 | B1 |
| Performance | ||
| Engine | 4x Aviadvigatel (Soloviev) PS-90A | 4x 4 × General Electric F101-GE-102 |
| Power, lbf (lbf) | 35,300 | 30,780 |
| Avionics | - | AN/APQ-164, AN/ALQ-161, AN/ASQ-184 |
| Max cruise speed (km/h) | 850 | 1,528 |
| Approach speed (km/h) | - | 463 |
| Travel range (km) | 11,499 | 12,010 |
| Fuel economy (km/l) | - | 0.078 |
| Service ceiling (m) | 13,106 | 18,288 |
| Rate of climb (m/sec) | - | 30.48 |
| Take off distance (m) | 2,380 | 600 |
| Landing distance (m) | 860 | 420 |
| Weights | ||
| Max take off weight (kg) | 250,000 | 216,634 |
| Max payload (kg) | 40,000 | 34,019 |
| Fuel tank capacity (l) | 152,635 | 149,875 |
| Dimensions | ||
| Seats | 24 | 4 |
| Cabin height (m) | 2.86 | - |
| Cabin width (m) | 5.7 | - |
| Cabin length (m) | 34.4 | - |
| Exterior length (m) | 55.3 | 44.8 |
| Tail height (m) | 15.7 | 10.4 |
| Fuselage diameter (m) | 6.08 | 2.6 |
| Wing span (m) | 60.1 | 41.8 |
| Wing tips | Canted Winglets | No Winglets |
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