Names and dates
Market original model designation | ЛК-2 | Market model designation (english translation or spelling) | LK-2 | Project start date | 1992 | Date of prototype completion | 1998 | Tests start date | 1997 | First flight date and time | 1998-03 | Country of manufacture | Ukraine |
People involved
Leonid Kozyarchuk {Леонід Козярчук} | Constructor |
Config info
Weights
Maximum Takeoff Weight (MTOW) | | Manufacturers empty weight (MEW) | |
Cabin and cockpit
Maximum number of people onboard | 1 |
External dimensions
Length | | Width | | Height | | Main landing gear wheel diameter | | Main landing gear wheel width | | Nose landing gear wheel diameter | | Nose landing gear wheel width | |
Control system
Rudder left deflection | | Rudder right deflection | |
Main rotor
Main rotor type | Semi-rigit | Cyclic control | Tilting rotor shaft | Main rotor diameter | | Number of blades | 2 | Main rotor blade chord | | Main rotor blade airfoil | NACA 8-H-12 |
Propeller
Propeller diameter | | Propeller material | Wood | Thrust | | Transmission reduction ratio | 2.13 |
Powerplant
Engine model | Custom MP-800B / IZ-P-3 | Engine dry weight with propeller | | Total maximum power | | Angular speed at max power | |
Fuel system
Performance
Maximum horizontal flight speed (Vh) | | Minimum speed | | Best rate of climb | |
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