Last site update: 03-10-2008

 

         

 

  

 

Mikoyan-Gurevich MiG-15bis

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Mikoyan-Gurevich MiG-15bis

The Mikoyan-Gurevich MiG-15 was extremely simple although advanced in concept. The MiG-15 was the Soviet Union’s first operational swept wing aircraft. It had a better rate of climb, ceiling and high-altitude radius of turn than any Allied jet aircraft at the time. It came as a shock to the American pilots who first encountered it in combat over Korea. Its appearance over Korea in late 1950 shattered the complacency of Western air forces that, until then, had dismissed Soviet fighters as second rate.

Conceived in 1947, the design lacked a suitable engine until the British Government made a gift of an example of their latest turbojet, the Rolls-Royce Nene, to the Soviet Union. It was immediately stripped and copied and went into production for the new fighter and within eight months the prototype MiG-15 was flying. Deliveries began in the winter of 1949 but early aircraft soon revealed various minor deficiencies that were corrected in the more powerful and robust MiG-15bis. By the time production ended, some 16.000 MiG-15s of all types had been built in the Soviet Union, Czechoslovakia, Poland and China. They served in almost forty countries.

A number of improvements were added to the MiG-15bis during production, including replacement of the NS-23 23-millimeter cannons with NP-23 23-millimeter cannons, providing a 50% higher rate of fire; a modified canopy providing a better field of view; cockpit pressurization bleed for a gee-suit; bigger dive brakes; more cockpit armor; a Sirena-2 radar warning system; and an electrical engine self-starting system, eliminating the need for a ground cart. A small number of MiG-15bis Fagot-Bs were built with a brake parachute and antiskid braking system, though this was not standard kit.

  • I-310 : Prototype.
  • MiG-15 : Single-seat jet fighter. The first production version.
  • MiG-15P : Single-seat all-weather interceptor version of the Mig-15bis.
  • MiG-15SB : Single-seat fighter bomber version.
  • MiG-15SP-5 : Two-seat all-weather interceptor version of the MiG-15UTI.
  • MiG-15T : Target-towing version.
  • MiG-15bis : Improved single-seat fighter version.
  • MiG-15bisR : Single-seat reconnaissance version.
  • MiG-15bisS : Single-seat escort fighter version.
  • MiG-15bisT : Single-seat target-towing version.
  • MiG-15UTI : Two-seat dual-control jet trainer.
  • J-2 : Chinese designation of the MiG-15 single-seat fighter.
  • JJ-2 : Chinese designation of the MiG-15UTI two-seat jet trainer.
  • Lim-1 : MiG-15 jet fighters built under licence in Poland.
  • Lim-1A : Polish built, reconnaissance version of MiG-15 with AFA-21 camera
  • Lim-2 : MiG-15bis built under licence in Poland.
  • Lim-2R : Polish-built ground attack-reconaissance version of MiG-15bis with place for camera in the front part of the canopy
  • Lim-2A : Polish build biplace ground attack-reconnaissance version
  • SB Lim-1 : MiG-15UTI with RD-45 engine jet trainers built under licence in Poland.
  • SB Lim-2 : MiG-15UTI with VK-1 jet trainers built under licence in Poland.
  • S-102 : MiG-15 jet fighters built under licence in Czechoslovakia.
  • S-103 : MiG-15bis jet fighters built under licence in Czechoslovakia.

Most MiG-15 family aircraft originally flew in natural metal colors, though there were some special bright paint jobs for airshow demonstration machines. In the late 1950s, many MiG-15bis fighters were shoehorned into the fighter-bomber role, being fitted with an additional stores pylon under each wing for carriage of a bomb or unguided rocket launcher. These machines were often painted in disruptive camouflage color schemes. Of course there were special color schemes, such as the overall red color for the "Red Five", and one American pilot even reported shooting down a MiG-15 during the Korean War that had a dragon painted along the full length of the fuselage!

 

 

Developing Nation: Soviet Union.
Manufacturer/Designer:  Mikoyan-Gurevich.
Task: Interceptor-Fighter.
First Flight:

- December 30, 1947 (S-01 MiG-15 I-310).

- September 1949 (MiG-15bis).

First Operational: End of 1951.
Crew:

- 1 MiG-15bis.

- 2 MiG-15UTI (tutorial).

Wing Span: 10,08 m.
Wing Area: 20,60 m².
Length: 10,86 m.
Height: 3,70 m.
Engine (s): 1x Klimov VK-1 (improved version of the RD-45F).
Weight: 3.681 kg.
Max. Take off weight: 5.580 kg.
Max. Speed:

- 1.076 km/h at sea level.

- 1.107 km/h at 3000 m.

Max. Range: 1.330 km (internal fuel only).
Hardpoint('s): 2x for 50 or 100 kg. bombs.
Weapons:

- 1x 37 mm. N37 cannon.

- 2x 23 mm. NS-23KM cannon.

 

 

 

 

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