Names and dates
| Market original model designation | KA-2HT | | Market model designation (english translation or spelling) | KA-2HT | | Project start date | | | Country of manufacture | Italy |
Config info
| Rotorcraft type | Helicopter |
Weights
| Maximum Takeoff Weight (MTOW) | | | Manufacturers empty weight (MEW) | |
Cabin and cockpit
| Maximum number of people onboard | 2 |
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 twist | | | Main rotor blade twist type | Nonlinear |
Propeller
Powerplant
| Engine model | K4A V2400–A2HT | | Engine type | Piston | | Number of engines | 2 | | Total maximum power | | | Angular speed at max power | |
Fuel system
| Fuel type | Automotive, 95 Oct. |
Performance
| Never exceed speed (Vne) | | | Maximum horizontal flight speed (Vh) | | | 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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