Rockwell B-1B Lancer [+]Compare [E]dit [H]istory
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Object «Rockwell B-1B Lancer» has attributes [Show empty attributes][Hide empty attributes]
| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Rockwell International |
| Model | Rockwell B-1B Lancer |
| Country | United States |
| Manufactured from | 1983 year |
| Manufactured to | 1988 year |
| Type | Military Aircraft |
| Icao | B1 |
| Performance | |
| Engine | 4x 4 × General Electric F101-GE-102 |
| Power, hp | Add |
| Power, lbf | 30,780 lbf |
| Avionics | AN/APQ-164, AN/ALQ-161, AN/ASQ-184 |
| Max cruise speed | 1,528 km/h |
| Approach speed | 463 km/h |
| Travel range | 12,010 km |
| Fuel economy | 0.078 km/l |
| Service ceiling | 18,288 m |
| Rate of climb | 30.48 m/sec |
| Take off distance | 600 m |
| Landing distance | 420 m |
| Weights | |
| Max take off weight | 216,634 kg |
| Max landing weight | Add |
| Max payload | 34,019 kg |
| Fuel tank capacity | 149,875 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 4 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 44.8 m |
| Tail height | 10.4 m |
| Fuselage diameter | 2.6 m |
| Wing span | 41.8 m |
| Wing tips | No Winglets |
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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (42 fields were changed)
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