Comparison of Mil Mi-34 “Hermit” and Rotorway A600 Talon [S]ave
| Attribute |  Mil Mi-34 “Hermit” × |  Rotorway A600 Talon × |
|---|---|---|
| General | ||
| Manufacturer | MIL Helicopters | Rotorway |
| Model | Mil Mi-34 “Hermit” | Rotorway A600 Talon |
| Country | Russia | United States |
| Manufactured from (year) | 1989 | 2007 |
| Type | Light Helicopters | Light Helicopters |
| Icao | - | A600 |
| Performance | ||
| Engine | 1 × Vedeneev M-14V-26 9-cylinder - | 1x 1 X Rotorway RI 600S other |
| Power, hp (hp) | 320 | 168 |
| Avionics | - | FADEC Glass Cockpit |
| Max cruise speed (km/h) | 170 | 161 |
| Travel range (km) | 450 | 304 |
| Fuel economy (km/l) | 2.945 | 4.726 |
| Service ceiling (m) | 4,499 | 3,353 |
| Rate of climb (m/sec) | 9.16 | 5.08 |
| Weights | ||
| Max take off weight (kg) | 1,350 | 739 |
| Max payload (kg) | 550 | 281 |
| Fuel tank capacity (l) | 174 | 64 |
| Baggage volume (m³) | 1 | - |
| Dimensions | ||
| Seats | 3 | 2 |
| Cabin width (m) | - | 1.1 |
| Exterior length (m) | 11.42 | 9 |
| Tail height (m) | - | 2.1 |
| Fuselage diameter (m) | - | 1.1 |
| Wing span (m) | 10.01 | 7.9 |
| Wing tips | No Winglets | No Winglets |
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