Deagostini – Pe-2 Petlyakov , ‘3’ Soviet Air Forces

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-sběratelský model letadla Pe-2 Petlyakov  délka modelu 10,0cm
-provedení: kovový model s plastovými částmi 

                        Petlyakov Pe-2

V létě roku 1938 dostala konstrukční kancelář V. M. Petljakova požadavek na konstrukci dvoumotorového rychlého výškového stíhacího letounu. K zalétání dvoumístného prototypu Petljakov VI-100 došlo 22. prosince 1939 pilotem P. M. Stěfanovským, avšak zkoušky ještě pokračovaly do května roku následujícího. Motory byly řadové dvanáctiválce V. K. Klimova M-105 po 772 kW s turbokompresory TK-3. Letoun měl zabudovány čtyři pevné kanóny ŠVAK ráže 20 mm, pozorovatel/radista ovládal jeden pohyblivý kulomet ŠKAS ráže 7,62 mm. Bylo však rozhodnuto další práce zastavit a na základě vyhodnocení bojů Luftwaffe v Polsku byl zadán požadavek na přeměnu stroje na střemhlavý bombardér.

The Petlyakov Pe-2 (Russian: Петляков Пе-2) was a Soviet twin-engined dive bomber used during World War II. It was regarded as one of the best front-line medium bomber of the war and it was also successful in the roles of heavy and night fighter (Pe-3 variant) as well as of reconnaissance aircraft. It was similar in many respects to the wooden British de Havilland Mosquito. Pe-2s were manufactured in greater numbers (11,430 built) during the war than any other twin-engined combat aircraft except for the German Junkers Ju 88 and British Vickers Wellington.The Pe-2 was fast, maneuverable and durable. Several Communist nations flew the type after the war, when it became known by the NATO reporting name Buck. Six captured Pe-2s were also transferred from the Germans to the Finnish Air Force during the Continuation War, with the serial code PE- and the unofficial nickname Pekka-Eemeli.

Role Dive bomber
National origin Soviet Union
Manufacturer Plant No.22 (Kazan), Plant No.39 (Moscow), Plant No.124 (Kazan), Plant No.125 (Irkutsk)
Designer V.M. Petlyakov Design Bureau
First flight 22 December 1939 (VI-100)
Introduction March 1941
Retired 1951 (Soviet Air Force), 1957 (Polish Air Force)
Primary users Soviet Air Force
Polish Air Force, Czechoslovakian Air Force, Bulgarian Air Force
Produced December 1940 – December 1945
Number built 11,070 (+ 360 Pe-3)
Variants Petlyakov Pe-3

General characteristics

  • Crew: Three – pilot, navigator, gunner
  • Length: 12.66 m (41 ft 6 in)
  • Wingspan: 17.16 m (56 ft 3 in)
  • Height: 3.5 m (11 ft 6 in)
  • Wing area: 40.5 m² (436 ft²)
  • Empty weight: 5,875 kg (12,952 lb)
  • Loaded weight: 7,563 kg (16,639 lb)
  • Max. takeoff weight: 8,495 kg (18,728 lb)
  • Powerplant: 2 × Klimov M-105 PF liquid-cooled V-12, 903 kW (1,210 hp) each

Performance

  • Maximum speed: 580 km/h (360 mph)
  • Range: 1,160 km (721 miles)
  • Service ceiling: 8,800 m (28,870 ft)
  • Rate of climb: 7.2 m/s (1,410 ft/min)
  • Wing loading: 186 kg/m² (38 lb/ft²)
  • Power/mass: 250 W/kg (0.15 hp/lb)

Armament

  • Guns:
    • 2 7.62 mm (0.3 in) fixed ShKAS machine guns in the nose, one replaced by a 12.7 mm (0.5 in) Berezin UB on later versions.
    • 2 rearward firing 7.62 mm (0.3 in) ShKAS machine guns.
    • From the middle of 1942 defensive armament included 1 Berezin UB machine gun in the upper bombardier’s turret, 1 Berezin UB in gunner’s ventral hatch and 1 ShKAS which could be fired by a gunner from port, starboard or upper mountings
    • Some planes were also equipped with a DAG-10 launcher, firing AG-2 parachute timed grenades.
  • Bombs: 1,600 kg (3,520 lb) of bombs

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