| Manufacturer | North American |
| Model | X-15 |
| Modification | X-15A |
| Country | USA |
| Years | 1959 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 6.71 m |
| Length | 15.24 m |
| Height | 4.12 m |
| Wing area | 18.58 m2 |
| Zero fuel weight | - |
| Empty weight | 6350 kg |
| Maximum takeoff weight | 15422 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 РД Reaction Motors (Thiokol) XLR99-RM-2 |
| Power | - |
| Thrust | 1 x 25855 kN |
| Maximum speed | 6600 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
