| Manufacturer | North American |
| Model | X-10 |
| Modification | X-10 |
| Country | USA |
| Years | 1953 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.58 m |
| Length | 21.64 m |
| Height | 4.42 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 10260 kg |
| Maximum takeoff weight | 18430 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 ТРД Westinghouse XJ40 |
| Power | - |
| Thrust | 2 x 4536 kN |
| Maximum speed | 2092 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 645 km |
| Service ceiling | 13716 m |
| Hovering ceiling | - |
| Crew | - |
