| Manufacturer | Rockwell |
| Model | B-1B Lancer |
| Modification | B-1B |
| Country | USA |
| Years | 1984 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 44.50 m |
| Height | 10.36 m |
| Wing area | 181.16 m2 |
| Zero fuel weight | - |
| Empty weight | 86183 kg |
| Maximum takeoff weight | 214650 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 4 General Electric F-101-GE-102 |
| Power | - |
| Thrust | - |
| Maximum speed | M=1.20 km/h |
| Cruising speed | M=0.95 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 18300 m |
| Hovering ceiling | - |
| Crew | 4 |
