| Technical data about the Rockwell B-1 Lancer | |
|---|---|
| Crew | 4 men |
| Length | 44.81 m |
| Span -spreaded -not spreaded |
41.76 m 23.77 m |
| Height | 10.36 m |
| Engines | four General Electric F101-GE-102 each with 136 kN thrust |
| Weapons | 34,000 kg weapons cruise missiles, bombs |
| Maximum speed | 1,450 km/h (1.2 Mach) |
| Maximum takeoff weight | 216,500 kg |
| Range | 12,000 km |