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McDonnell Douglas F-4 Phantom II Supersonic Aircraft Family

The McDonnell Douglas F-4 Phantom II is a two-seat, twin-engine supersonic aircraft family that first flew in 1958. Developed by McDonnell for U.S. Navy fleet defense, it expanded into a widely operated family for air defense, reconnaissance, training, electronic-warfare, and other military duties. National and service variants introduced different sensors, structures, and engine installations while retaining the common Phantom II design.

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Identity

Aliases
McDonnell F4H Phantom IIF4H-1F-4 Phantom IIF-4BF-4CF-4DF-4EF-4EJF-4FF-4GF-4JF-4KF-4MF-4NF-4SFG.1 PhantomFGR.2 PhantomRF-4CRF-4EQF-4
Family Name
McDonnell Douglas F-4 Phantom II
Full Name
McDonnell Douglas F-4 Phantom II Supersonic Aircraft Family
Roles
militaryreconnaissancetrainerresearch
Status
active
Type
aircraft

Details

Aircraft Specs
Configuration
fixed_wing
Operating Modes
land
Takeoff Landing Capabilities
conventional
Description
The McDonnell Douglas F-4 Phantom II is a two-seat, twin-engine supersonic aircraft family that first flew in 1958. Developed by McDonnell for U.S. Navy fleet defense, it expanded into a widely operated family for air defense, reconnaissance, training, electronic-warfare, and other military duties. National and service variants introduced different sensors, structures, and engine installations while retaining the common Phantom II design.
First Flight Year
1,958
Manufacturer
Propulsion Configurations
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Variant Notes
      Two General Electric J79 turbojets; representative variants include J79-GE-8, -10, -15, and -17 installations.
    Name
    J79-powered Phantom II variants
    Notes
    Applies to the principal U.S. and most export Phantom II variants; exact J79 dash number and rating vary by variant.
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Variant Notes
      Two Rolls-Royce RB.168 Spey afterburning turbofans, using Spey 201/202 installations across the British variants.
    Name
    British Spey-powered Phantom variants
    Notes
    Applies to the Royal Navy F-4K/FG.1 and Royal Air Force F-4M/FGR.2.
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Variant Notes
      The U.S. Air Force/ANG fact sheet identifies two General Electric J79-GE-17 engines on the F-4E; GE rates the J79-17 at approximately 17,900 lbf with afterburner.
    Name
    F-4E Phantom II J79-GE-17 installation
  • Entries
    • Count
      2
      Propulsion System
      Role
      main
      Variant Notes
      RAF Museum collections identify Rolls-Royce R.B.168-25R Spey 202 as fitted to RAF Phantom FGR.2 aircraft; this exact model option is scoped to the British FGR.2 branch, while placement and stage are not inferred from the exhibit record.
    Name
    FGR.2 Phantom Spey 202 exact installation
    Notes
    The RAF Museum identifies the British Phantom FGR.2 as Spey-powered and separately catalogs an R.B.168-25R Spey 202 engine fitted to RAF Phantom FGR.2 aircraft. This model-level option supplements the existing generic British Spey family configuration without collapsing the exact variant boundary.
  • Entries
    • Count
      2
      Propulsion System
      Role
      main
      Variant Notes
      The National Museum of the United States Air Force identifies the F-4C with two General Electric J-79-GE-15 engines at 17,000 lb thrust each. Placement and stage are left unspecified because the cited aircraft record does not state them.
    Name
    F-4C Phantom II J79-GE-15 exact installation
    Notes
    Exact F-4C branch: the National Museum of the United States Air Force identifies two General Electric J-79-GE-15 engines at 17,000 lb thrust each. This exact option supplements the generic J79 branch and does not apply to F-4E or British Spey variants.
  • Entries
    • Count
      2
      Propulsion System
      Role
      main
      Variant Notes
      The Smithsonian National Air and Space Museum identifies the basic F-4B as powered by two 17,000-lb-thrust J79-GE-8 turbojets; Naval History and Heritage Command identifies F4H-1 (F-4B) with the J79-GE-8 engine. Placement and stage are left unspecified because the cited records do not state them.
    Name
    F-4B Phantom II J79-GE-8 exact installation
    Notes
    Exact basic F-4B branch: the Smithsonian National Air and Space Museum and Naval History and Heritage Command identify two General Electric J79-GE-8 turbojets. This exact option supplements the generic J79 branch and does not apply to F-4C, F-4E, or British Spey variants.
  • Entries
    • Count
      2
      Propulsion System
      Role
      main
      Variant Notes
      Pima Air & Space Museum identifies the F-4J/YF-4J record with two General Electric J79-GE-10 turbojets at 17,900 lb thrust each; the Department of Defense record independently associates J79-GE-10 with F-4J. Placement and stage are left unspecified because the cited records do not state them.
    Name
    F-4J Phantom II J79-GE-10 exact installation
    Notes
    Exact F-4J branch: Pima Air & Space Museum identifies two General Electric J79-GE-10 turbojets at 17,900 lb thrust each, with a Department of Defense engine record providing an independent F-4J association. This exact option supplements the generic J79 branch and does not apply to F-4B, F-4C, F-4E, or British Spey variants.

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Creation Time
July 30, 2026 at 04:00:22 UTC
Updated Time
August 25, 2026 at 04:26:38 UTC
McDonnell Douglas F-4 Phantom II Supersonic Aircraft Family - AeroVia