| Technical data | |
|---|---|
| Type | Pe-2VI |
| Function | Fighter |
| Year | 1943 |
| Crew | 1 |
| Engines | 2*1170hp VK-105PD |
| Length | 12.6m |
| Wingspan | 13.57m |
| Wing area | 40.5m2 |
| Empty weight | 5790kg |
| Loaded weight | 6870kg |
| Wing Load (kg/m2) | 170 |
| Power load (kg/hp) | 2.94 |
| Maximum Speed | (557km/h) |
| Ceiling | 10500m |
| Climb | |
| 5000m | (10.4min) |
| Armament | |
| Guns | ? |
Pe-2VI, modification by A.I.Putilov
Single-seat high altitude interceptor, developed from Pe-2 bomber by A.I.Putilov. Aircraft was equipped by pressurized cockpit designed by A.I.Putilov. It was actually a whole nose section, wielded of aluminum-magnesium alloy on internal frame.
New VK-105PD engine with high altitude superchargers (design by V.A.Dollezhal) supposed to push Pe-2VI to 12000m altitude, but failed. Aircraft was returned to factory for modification.
It was also tried with similar pressurized cabin by A.Ya.Scherbakov.
Remained experimental.
| Predecessors | Modifications |
|---|---|
 Pe-2 |
None |
| References | Links |
|---|---|
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