| Manufacturer | Rockwell |
| Model | B-1A Lancer |
| Modification | B-1A |
| Country | USA |
| Years | 1974 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 45.78 m |
| Height | 10.24 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | - |
| Maximum takeoff weight | 179170 kg |
| Normal takeoff weight | 176810 kg |
| Flight duration | - |
| Engine | 4 General Electric F-101-GE-100 |
| Power | - |
| Thrust | 4 x 13500 kN |
| Maximum speed | - |
| Cruising speed | 900-1040 km/h |
| Rate of climb | - |
| Practical range | 9820 km |
| Service ceiling | 18300 m |
| Hovering ceiling | - |
| Crew | 4 |
