| Manufacturer | Rogerson Hiller |
| Model | RH-1100 Hornet |
| Modification | RH-1100 |
| Country | USA |
| Years | 1966 |
| Type | Helicopter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 9.08 m |
| Height | 2.79 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 766 kg |
| Maximum takeoff weight | 1588 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Allison 250-C20R |
| Power | 1 x 336 HP |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 216 km/h |
| Rate of climb | 546 m/min |
| Practical range | - |
| Service ceiling | 5790 m |
| Hovering ceiling | 4990 m |
| Crew | 1 |
