| Manufacturer | Engineering Division |
| Model | VCP-1 |
| Modification | VCP-1 |
| Country | USA |
| Years | 1919 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.75 m |
| Length | 6.81 m |
| Height | 2.54 m |
| Wing area | 24.99 m2 |
| Zero fuel weight | - |
| Empty weight | 913 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1211 kg |
| Flight duration | - |
| Engine | 1 Packard 1A-2025 |
| Power | 1 x 660 HP |
| Thrust | - |
| Maximum speed | 248 km/h |
| Cruising speed | 215 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
