Names and dates
| Market original model designation | АК-2 | | Market model designation (english translation or spelling) | AC-2 | | Project start date | 1988 | | Mockup construction date | 1991 | | Country of manufacture | Moldova |
People involved
| Alexander Satarov {Александр Сатаров} | Design engineer | | V. Goltsman {В. Гольцман} | Design engineer |
Config info
| Rotorcraft type | Autogyro | | Config | Single rotor |
Weights
| Maximum Takeoff Weight (MTOW) | |
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 | |
Main rotor
| Main rotor type | Semi-rigit | | Collective control | Yes | | Main rotor diameter | | | Main rotor direction of rotation | | | Prerotation type | Mechanical | | Number of blades | 2 | | Main rotor blade chord | |
Propeller
| Mode (System no.: 1) | Pushing | | Mode (System no.: 2) | Pushing | | Number of blades (System no.: 1) | 2 | | Number of blades (System no.: 2) | 2 | | Propeller material (System no.: 1) | Wood | | Propeller material (System no.: 2) | Wood |
Powerplant
| Engine model | P-032 {П-032} | | Engine type | Piston | | Number of engines | 2 | | Total maximum power | | | Angular speed at max power | |
Fuel system
| Fuel tank capacity [mass] | |
Performance
| Maximum horizontal flight speed (Vh) | | | Minimum speed | | | Take-off distance | | | Landing distance | | | Best rate of climb | | | Maximum flight endurance | |
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