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Mig-17

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MiG-17 fighter (Russian: mkk-17) is a single seat high subsonic fighter developed by mikoyang Design Bureau of the Soviet Union in the late 1940s.

The fighter is developed on the basis of mig-15bis. It adopts swept wing conventional aerodynamic layout, single engine, single seat, thrust to weight ratio of 0.57. It is equipped with one 37mm machine gun and two 23mm machine guns, with a maximum flying speed of 1100 km / h and a range of 2000 km.

The MiG-17 fighter plane was designed in 1948, began to test flight in December 1949, and entered the service of the former Soviet air force in 1952. The MiG-17 has several improved models, of which the most important type is the mig-17f daytime fighter and radar equipped with all-weather combat capability. A total of 10367 MiG-17 models were manufactured. In addition to the production in the Soviet Union, China, Poland and Czech Republic are authorized to copy mass production, so there are many derivative models. The MiG-17 was gradually retired and replaced by supersonic MiG-19 fighters.

AG1: acceleration

Ag2: Aiming

Ag3: ejection

AG4: parachute

Ag5: Weapons

General Characteristics

  • Successors 2 airplane(s)
  • Created On Windows
  • Wingspan 48.0ft (14.6m)
  • Length 55.1ft (16.8m)
  • Height 19.0ft (5.8m)
  • Empty Weight N/A
  • Loaded Weight 39,408lbs (17,875kg)

Performance

  • Power/Weight Ratio 2.737
  • Wing Loading 9.1lbs/ft2 (44.5kg/m2)
  • Wing Area 4,321.7ft2 (401.5m2)
  • Drag Points 11539

Parts

  • Number of Parts 402
  • Control Surfaces 5
  • Performance Cost 1,564