I-29, A.S.YakovlevF ighter version of the Ya-22. It had same folding
fuselage top behind the gunner position as Ya-22 and R-12 to allow unrestricted
gunner's operations and keep clean aerodynamics when there is no rear threat.
| Technical data | |
|---|---|---|
| Year | 1939 | |
| Function | Fighter | |
| Crew | 2 | |
| Engine | 2x960hp Klimov M-103 | |
| Empty Weight | 3,796kg | |
| Take off Weight | 5,023kg | |
| Wing Span | 14.0m | |
| Wing Area | 29.4m2 | |
| Length | 10.18m | |
| Speed | 567km/h | |
| Climb | 5000m 5.75min | |
| Range | 1,050km | |
| Ceiling | 10,800m | |
| Armament | 2mg7.62mm
2g20mm ShVAKunder fuselage with ammo in the bomb bay. | |
| Modified April 10, 1996
by Alexandre Savine; |
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