Comparison of Aérospatiale-BAC Concorde and Rockwell B-1B Lancer [S]ave
| Attribute |  Aérospatiale-BAC Concorde × |  Rockwell B-1B Lancer × |
|---|---|---|
| General | ||
| Manufacturer | Aérospatiale | Rockwell International |
| Model | Aérospatiale-BAC Concorde | Rockwell B-1B Lancer |
| Country | France | United States |
| Manufactured from (year) | 1965 | 1983 |
| Manufactured to (year) | 1979 | 1988 |
| Type | Mid Size Passenger Jets | Military Aircraft |
| Icao | CONC | B1 |
| Performance | ||
| Engine | 4x 4 × Rolls-Royce/SNECMA Olympus 593 Mk 610 | 4x 4 × General Electric F101-GE-102 |
| Power, lbf (lbf) | 38,050 | 30,780 |
| Avionics | Fly by wire flight controls, Digital Air Intake Control Units | AN/APQ-164, AN/ALQ-161, AN/ASQ-184 |
| Max cruise speed (km/h) | 2,330 | 1,528 |
| Approach speed (km/h) | 306 | 463 |
| Travel range (km) | 7,223 | 12,010 |
| Fuel economy (km/l) | 0.059 | 0.078 |
| Service ceiling (m) | 18,288 | 18,288 |
| Rate of climb (m/sec) | 25.4 | 30.48 |
| Take off distance (m) | 3,429 | 600 |
| Landing distance (m) | 2,200 | 420 |
| Weights | ||
| Max take off weight (kg) | 185,070 | 216,634 |
| Max payload (kg) | 11,000 | 34,019 |
| Fuel tank capacity (l) | 119,178 | 149,875 |
| Baggage volume (m³) | 6.71 | - |
| Dimensions | ||
| Seats | 128 | 4 |
| Seats - business class | 12 | - |
| Seats - first class | 92 | - |
| Cabin height (m) | 1.96 | - |
| Cabin width (m) | 2.63 | - |
| Cabin length (m) | 39.32 | - |
| Exterior length (m) | 61.66 | 44.8 |
| Tail height (m) | 12.2 | 10.4 |
| Fuselage diameter (m) | 2.87 | 2.6 |
| Wing span (m) | 25.6 | 41.8 |
| Wing tips | No Winglets | No Winglets |
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