Names and dates
| Market original model designation | СВ-2 | | Market model designation (english translation or spelling) | SV-2 | | Approximated date of prototype completion | Late 1980's | | Tests start date | 1989-05 | | Country of manufacture | Russia |
People involved
| Vasily Sverbil {Василий Свербиль} | Constructor |
Config info
| Rotorcraft type | Helicopter | | Config | Single rotor | | Way of counteracting main rotor torque | Tail rotor |
Weights
| Maximum Takeoff Weight (MTOW) | | | Manufacturers empty weight (MEW) | |
Cabin and cockpit
| Maximum number of people onboard | 1 |
External dimensions
| Fuselage length | | | Width | | | Height | | | Main landing gear wheel diameter | | | Nose landing gear wheel diameter | |
Main rotor
| Main rotor type | Fully articulated | | Main rotor diameter | | | Main rotor direction of rotation | Clockwise | | Max main rotor angular speed in prerotation | | | Number of blades | 3 |
Tail rotor
| Tail rotor type | Classic tail rotor | | Tail rotor diameter | | | Tail rotor direction of rotation | Clockwise | | Tail rotor angular speed | | | Number of blades | 2 | | Tail rotor arm | |
Powerplant
| Engine model | Walter M-332 | | Number of engines | 1 | | Total maximum power | | | Angular speed at max power | |
Performance
| Cruise speed (Vc) | | | Maximum service ceiling | | | Hover ceiling OGE | | | Maximum flight endurance | |
|
