| Manufacturer | Gloster |
| Model | CXP-1001 |
| Modification | CXP-1001 |
| Country | United Kingdom |
| Years | - |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.40 m |
| Length | 12.50 m |
| Height | - |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | - |
| Maximum takeoff weight | 6300 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 ТРД Rolls-Royce Nene |
| Power | - |
| Thrust | 1 x kN |
| Maximum speed | 970 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1600 km |
| Service ceiling | 12000 m |
| Hovering ceiling | - |
| Crew | - |
