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
5000m (10.4min)
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.



  • "History of aircraft construction in the USSR", Vol.2 p.162;
  • Pe-2 at Greg Goebel's Vectors

  • Created February 2, 1999 Back to
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