Manicatide RM-9
General information
| Manufacturer | Manicatide |
| Model | RM-9 |
| Modification | RM-9 |
| Country | Romania |
| Years | 1942 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 7.50 m |
| Length | 5.50 m |
| Height | - |
| Wing area | 9.00 m2 |
| Zero fuel weight | - |
| Empty weight | 255 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 350 kg |
| Flight duration | - |
| Engine | 1 Praga |
| Power | 1 x 32 HP |
| Thrust | - |
| Maximum speed | 138 km/h |
| Cruising speed | 110 km/h |
| Rate of climb | - |
| Practical range | 1000 km |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |