• HOME
  • 2017 Military Pay Chart
  • Military Pay Charts
  • Military Ranks
  • Military Time
  • Military Alphabet Code
  • Aviation Central
  • Land Systems
  • Warfighter (Small Arms)
  • Special Forces Equipment
  • Naval Firepower
  • World War 1 Weapons
  • World War 2 Weapons

  • Petlyakov VI-100 Heavy Twin-Engine Interceptor Prototype Aircraft


    The Petlyakov VI-100 heavy interceptor was a well-armed and aerodynamically-refined aircraft for its time but changing requirements for the Soviet Air Force led to its rebirth as the Pe-2 dive bomber.

     Updated: 5/7/2017; Authored By Staff Writer; Content ¬©www.MilitaryFactory.com


    There were only a handful of truly exceptional twin-engine heavy fighters fielded during World War 2 (1939-1945) - the British de Havilland "Mosquito" and American Lockheed "Lightning" quickly come to mind and these were joined by others such as the German Messerschmitt Bf 110, which found its success early in the war, and the Japanese went on to manufacture a plethora of twin-engined types for their part in the grand conflict. The Petlyakov concern of the Soviet Union eventually contributed its Pe-2 dive bomber of 1941 but this platform had origins in a potent design intended as a high-altitude interceptor in the pre-war years.

    Born as the "VI-100", the aircraft was expected to fulfill a growing need within the Soviet Air Force to counter high-flying enemy threats of the period - primarily bombers. Design work began in 1938 and the resulting design became a well-streamlined, twin-seat, all-metal, twin-engine offering. The crew of two were seated in line in separate cockpits (back-to-back). The wings were of monoplane arrangement and each held an engine nacelle at their leading edge. The tail was of a split-rudder configuration and the undercarriage of a "tail-dragger" form consistent with the period. The pilot's position was aft of a short nosecone containing a bulk of the offensive armament with defensive armament handled by the rear crewman. The pilot's cockpit was to be pressurized for high-altitude service. The powerplant of choice became 2 x Klimov M-105 inline piston engines of 1,050 horsepower. For the required high-altitude performance, these were fitted with turbo-superchargers.


    Images Gallery


    VIEW
    VIEW

    Petlyakov VI-100 Technical Specifications


    Service Year: 1940
    Type: Heavy Twin-Engine Interceptor Prototype Aircraft
    National Origin: Soviet Union
    Manufacturer(s): Petlyakov - Soviet Union
    Production Total: 1



    Structural (Crew Space, Dimensions and Weights)


    Operating Crew: 2
    Length: 41.01 feet (12.5 meters)
    Width: 56.30 feet (17.16 meters)
    Height: 11.48 feet (3.50 meters)

    Weight (Empty): 11,905 lb (5,400 kg)
    Weight (MTOW): 16,006 lb (7,260 kg)

    Installed Power and Standard Day Performance


    Engine(s): 2 x Klimov M-105 turbocharged inline piston engines developing 1,050 horsepower each.

    Maximum Speed: 332 mph (535 kph; 289 knots)
    Maximum Range: 870 miles (1,400 km)
    Service Ceiling: 40,026 feet (12,200 meters; 7.58 miles)
    Rate-of-Climb: 2,415 feet-per-minute (736 m/min)

    Armament / Mission Payload


    2 x 20mm ShVAK cannons in fixed, forward-firing position at nose.
    2 x 7.62mm ShKAS machine guns in fixed, forward-firing position at nose.
    1 x 7.62mm ShKAS machine gun on flexible mount in rear cockpit.

    OPTIONAL:
    Coventional drop bombs and rockets held at underwing racks.

    Global Operators / Customers


    Soviet Union (cancelled)

    Model Variants (Including Prototypes)


    VI-100 - Base Series Designation; single prototype completed.