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X-31 Enhanced Fighter Maneuverability Demonstrator Research Aircraft Family

The X-31 Enhanced Fighter Maneuverability demonstrator family comprised two international research aircraft flown by NASA, the U.S. Navy, the U.S. Air Force, Rockwell Aerospace, and German partners to test thrust-vectoring and advanced digital flight controls in the post-stall regime. The first aircraft flew in 1993 and was lost in 1995; the program logged 580 research and demonstration flights before concluding in June 1995, with the surviving aircraft continuing follow-on research and later entering a German museum collection.

X-31 Enhanced Fighter Maneuverability Demonstrator Research Aircraft Family
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Identity

Aliases
X-31Enhanced Fighter Maneuverability (EFM) DemonstratorX-31 Enhanced Fighter Maneuverability
Family Name
X-31 Enhanced Fighter Maneuverability Demonstrator
Full Name
X-31 Enhanced Fighter Maneuverability Demonstrator Research Aircraft Family
Roles
militaryresearchexperimentaltechnology_demonstrator
Status
retired
Type
aircraft

Details

Aircraft Specs
Configuration
fixed_wing
Operating Modes
land
Takeoff Landing Capabilities
conventional
Description
The X-31 Enhanced Fighter Maneuverability demonstrator family comprised two international research aircraft flown by NASA, the U.S. Navy, the U.S. Air Force, Rockwell Aerospace, and German partners to test thrust-vectoring and advanced digital flight controls in the post-stall regime. The first aircraft flew in 1993 and was lost in 1995; the program logged 580 research and demonstration flights before concluding in June 1995, with the surviving aircraft continuing follow-on research and later entering a German museum collection.
First Flight Year
1,993
Last Flight Year
1,995
Propulsion Configurations
  • Entries
    • Count
      1
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      Single F404-GE-400 installation; NASA reports 16,000 lbf / approximately 71.17 kN afterburning thrust. Exact thrust-vectoring paddles are installation hardware, not separate propulsion identities.
    Name
    X-31 single-engine F404-GE-400 thrust-vectoring installation
    Notes
    The X-31 demonstrators used one General Electric F404-GE-400 turbofan. Three carbon-carbon thrust-vectoring paddles adjacent to the engine nozzle redirected exhaust in pitch and yaw, coupled with digital flight controls for high-angle-of-attack and post-stall maneuvering.

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Creation Time
August 13, 2026 at 21:22:38 UTC
Updated Time
September 8, 2026 at 10:06:04 UTC