| Manufacturer | Bristol |
| Model | Braemar |
| Modification | Braemar I |
| Country | United Kingdom |
| Years | 1918 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 24.89 m |
| Length | 15.70 m |
| Height | 6.30 m |
| Wing area | 176.97 m2 |
| Zero fuel weight | - |
| Empty weight | 5084 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 7490 kg |
| Flight duration | - |
| Engine | 4 Armstrong Siddeley Puma |
| Power | 4 x 230 HP |
| Thrust | - |
| Maximum speed | 170 km/h |
| Cruising speed | 142 km/h |
| Rate of climb | - |
| Practical range | 2000 km |
| Service ceiling | 5180 m |
| Hovering ceiling | - |
| Crew | - |
