| Manufacturer | Fouga |
| Model | CM.88 Gemeaux |
| Modification | СM.88-R |
| Country | France |
| Years | 1951 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.76 m |
| Length | 6.66 m |
| Height | 1.93 m |
| Wing area | 12.80 m2 |
| Zero fuel weight | - |
| Empty weight | 724 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1080 kg |
| Flight duration | 1.30 h |
| Engine | 2 ТРД Turbomeca Pimene |
| Power | - |
| Thrust | 2 x 111 kN |
| Maximum speed | 330 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 9500 m |
| Hovering ceiling | - |
| Crew | 2 |
