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Mikoyan-Gurevich MiG-21 Supersonic Aircraft Family

The Mikoyan-Gurevich MiG-21 is a single-engine supersonic aircraft family whose early prototype first flew in 1955. Its compact tailed-delta layout became one of the most widely produced and internationally operated jet-aircraft designs. Successive interceptor, multi-role, reconnaissance, and two-seat training variants introduced new radar, systems, and Tumansky engine generations while retaining the recognizable MiG-21 architecture.

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Identity

Aliases
MiG-21МиГ-21Ye-4E-4FishbedMiG-21FMiG-21F-13MiG-21PFMiG-21PFMMiG-21SMiG-21MMiG-21MFMiG-21SMTMiG-21bisMiG-21UMiG-21UMMiG-21 Bison
Family Name
Mikoyan-Gurevich MiG-21
Full Name
Mikoyan-Gurevich MiG-21 Supersonic Aircraft Family
Roles
militaryreconnaissancetrainer
Status
active
Type
aircraft

Details

Aircraft Specs
Configuration
fixed_wing
Operating Modes
land
Takeoff Landing Capabilities
conventional
Description
The Mikoyan-Gurevich MiG-21 is a single-engine supersonic aircraft family whose early prototype first flew in 1955. Its compact tailed-delta layout became one of the most widely produced and internationally operated jet-aircraft designs. Successive interceptor, multi-role, reconnaissance, and two-seat training variants introduced new radar, systems, and Tumansky engine generations while retaining the recognizable MiG-21 architecture.
First Flight Year
1,955
Manufacturer
Propulsion Configurations
  • Entries
    • Count
      1
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      One exact R-25-300 afterburning turbojet; UEC/Rostec MiG-21BIS installation evidence.
    Name
    MiG-21BIS exact R-25-300 configuration
    Notes
    UEC/Rostec identifies R-25-300 for the MiG-21BIS fighter; this configuration applies only to the MiG-21BIS branch and does not infer other MiG-21 variants.
  • Entries
    • Count
      1
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      One exact R-13-300 afterburning turbojet; UEC/Rostec MiG-21 application evidence.
    Name
    MiG-21 exact R-13-300 configuration
    Notes
    UEC/Rostec identifies R13-300 for MiG-21 variants; this family-level option does not infer a narrower MiG-21 submodel or the separate Su-15 applications.

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Creation Time
July 30, 2026 at 04:09:04 UTC
Updated Time
August 14, 2026 at 15:51:02 UTC