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NASA F-18 High Alpha Research Vehicle

The F-18 High Alpha Research Vehicle was a heavily modified Hornet used to study control at very high angles of attack. NASA’s three flight-research phases ran from April 1987 through September 1996. Initial flow visualisation and aerodynamic measurements were followed by exhaust-deflecting thrust-vector vanes and a research flight-control system, then actuated forebody strakes. Across 385 research flights, the aircraft demonstrated stabilised flight at angles of attack of 65–70 degrees. The thrust-vector installation removed the divergent nozzle sections and prevented supersonic flight in that configuration. Flight measurements helped validate wind-tunnel results and computational fluid-dynamics predictions.

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Identity

Aliases
F-18 HARVHigh Alpha Research VehicleHigh Angle-of-Attack Research Vehicle
Family Name
McDonnell Douglas F/A-18 Hornet
Full Name
NASA F-18 High Alpha Research Vehicle
Roles
researchexperimentaltechnology_demonstrator
Status
retired
Type
aircraft
Variant Name
High Alpha Research Vehicle

Details

Aircraft Specs
Configuration
fixed_wing
Crew Capacity
1
Operating Modes
land
Takeoff Landing Capabilities
conventional
Description
The F-18 High Alpha Research Vehicle was a heavily modified Hornet used to study control at very high angles of attack. NASA’s three flight-research phases ran from April 1987 through September 1996. Initial flow visualisation and aerodynamic measurements were followed by exhaust-deflecting thrust-vector vanes and a research flight-control system, then actuated forebody strakes. Across 385 research flights, the aircraft demonstrated stabilised flight at angles of attack of 65–70 degrees. The thrust-vector installation removed the divergent nozzle sections and prevented supersonic flight in that configuration. Flight measurements helped validate wind-tunnel results and computational fluid-dynamics predictions.
Dimensions
Length
…
Wingspan
…
First Flight Year
1,987
Last Flight Year
1,996
Manufacturer
Operator
Parent Vehicle Family
Propulsion Configurations
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Variant Notes
      In the thrust-vectoring research configuration, external vanes deflected engine exhaust and the divergent nozzle sections were removed.
    Name
    HARV twin F404-GE-400 installation

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Creation Time
October 29, 2026 at 16:05:00 UTC
Updated Time
October 29, 2026 at 16:05:00 UTC