Names and dates
| Approximated date of prototype completion | Early 1990's | | Country of manufacture | Russia |
People involved
| A. Tatarnikov {А. Татарников} | Design engineer | | I. Shirokov {И. Широков} | Design engineer | | G. Galkevich {Г. Галькевич} | Design engineer | | Andrei Sysolyatin {Андрей Сысолятин} | Test pilot |
Config info
Weights
| Manufacturers empty weight (MEW) | |
Cabin and cockpit
| Maximum number of people onboard | 2 |
External dimensions
| Main landing gear wheel diameter | | | Main landing gear wheel width | | | Nose landing gear wheel diameter | | | Nose landing gear wheel width | |
Main rotor
| Cyclic control | Tilting rotor shaft | | Main rotor diameter | | | Prerotation | No | | Main rotor blade mass | |
Propeller
| Mode | Pushing | | Number of blades | 3 | | Thrust | |
Powerplant
| Engine model | | | Engine model (english translation or spelling) | | | Engine type | Piston | | Number of engines | 1 | | Total maximum power | |
Fuel system
Performance
| Maximum horizontal flight speed (Vh) | | | Cruise speed (Vc) | | | Best endurance speed (Vbe) | | | Take-off distance | | | Landing distance | |
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