| /Airplanes/Allies/USSR/01-Fighters/OI-2/OI-2.htm / | Up-dated: 25-04-2025 |
| /Airplanes/Allies/USSR/01-Fighters/OI-2/OI-2.htm / | Up-dated: 25-04-2025 |
Project designed
in 1941-1942. The single-seater Byelyayev OI-2 (maybe Odnomyestniy Istribityel 2-motorniy) used the central-engined fuselage of the P-39 Airacobra, doubled and adapted. The central wing housed a load bay. |
Specifications |
| General |
Type: Fighter |
| Engine |
| 2 x M-120UV 18 | 2 x 1800 hp | Pistons |
| Dimensions/Masses |
| Length: 12 m | Width: 15 m | Height: 4 m Weight: ? kg | Max. Combat Weight: 6800kg |
| Performances |
| Max. Speed: 780km/h
| Ceiling: ? m Range: 1000km/1400km |
| Armament |
MG: 2 x 23mm MP-6 + 4 x 12.7mm BS + 4 x 7.62mm ShKAS |
