Comparison of Boeing B-52 Stratofortress and Rockwell B-1B Lancer [S]ave
| Attribute |  Boeing B-52 Stratofortress × |  Rockwell B-1B Lancer × |
|---|---|---|
| General | ||
| Manufacturer | Boeing | Rockwell International |
| Model | Boeing B-52 Stratofortress | Rockwell B-1B Lancer |
| Country | United States | United States |
| Manufactured from (year) | 1952 | 1983 |
| Manufactured to (year) | 1962 | 1988 |
| Type | Military Aircraft | Military Aircraft |
| Icao | B52 | B1 |
| Performance | ||
| Engine | 8x Pratt & Whitney TF33-P-3/103 | 4x 4 × General Electric F101-GE-102 |
| Power, lbf (lbf) | 17,000 | 30,780 |
| Avionics | AN/ASQ, AN/ASQ-151 EVS, IBM AP-101 | AN/APQ-164, AN/ALQ-161, AN/ASQ-184 |
| Max cruise speed (km/h) | 1,037 | 1,528 |
| Approach speed (km/h) | - | 463 |
| Travel range (km) | 14,172 | 12,010 |
| Fuel economy (km/l) | - | 0.078 |
| Service ceiling (m) | 15,240 | 18,288 |
| Rate of climb (m/sec) | 31.85 | 30.48 |
| Take off distance (m) | 3,000 | 600 |
| Landing distance (m) | 3,000 | 420 |
| Weights | ||
| Max take off weight (kg) | 220,000 | 216,634 |
| Max payload (kg) | 31,500 | 34,019 |
| Fuel tank capacity (l) | 181,605 | 149,875 |
| Dimensions | ||
| Seats | 5 | 4 |
| Exterior length (m) | 48.5 | 44.8 |
| Tail height (m) | 12.4 | 10.4 |
| Fuselage diameter (m) | 2.8 | 2.6 |
| Wing span (m) | 56.4 | 41.8 |
| Wing tips | No Winglets | No Winglets |
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