| Manufacturer | Curtiss |
| Model | X-100 |
| Modification | X-100 |
| Country | USA |
| Years | 1960 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 8.64 m |
| Height | 3.28 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 1481 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1691 kg |
| Flight duration | - |
| Engine | 1 Lycoming YT53-L-1 |
| Power | 1 x 825 HP |
| Thrust | - |
| Maximum speed | 386 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
