Names and dates
| Market original model designation | Voyager-500 | | Market model designation (english translation or spelling) | Voyager-500 | | First flight date and time | 1998-09-21 15:05 |
Config info
| Rotorcraft type | Helicopter |
Weights
| Maximum Takeoff Weight (MTOW) | | | Manufacturers empty weight (MEW) | |
Cabin and cockpit
| Maximum number of people onboard | 2 |
External dimensions
| Fuselage length | | | Height | | | Total length (rotors turning) | | | Landing gear width | |
Main rotor
| Main rotor type | Semi-rigit | | Main rotor diameter | | | Main rotor angular speed | | | Number of blades | 2 | | Main rotor blade chord | | | Main rotor blade airfoil | 12.5% | | Main rotor blade twist | | | Main rotor blade twist type | Linear |
Tail rotor
| Tail rotor type | Classic tail rotor | | Tail rotor diameter | | | Tail rotor angular speed | | | Pre-coning angle | | | Tail rotor blade chord | |
Powerplant
| Engine model | U.S.Air Power Inc. H1300 | | Engine type | Piston | | Total maximum power | | | Angular speed at max power | |
Fuel system
Performance
| Never exceed speed (Vne) | | | Cruise speed (Vc) | | | Best rate of climb | | | Miminum rate of descend in autorotation | | | Maximum service ceiling | | | Hover ceiling IGE | | | Hover ceiling OGE | | | Maximum range | | | Maximum flight endurance | |
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