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The F-18 High Alpha Research Vehicle - A high-angle-of-attack testbed aircraftThe F-18 High Alpha Research Vehicle is the first thrust-vectoring testbed aircraft used to study the aerodynamics and maneuvering available in the poststall flight regime and to provide the data for validating ground prediction techniques. The aircraft includes a flexible research flight control system and full research instrumentation. The capability to control the vehicle at angles of attack up to 70 degrees is also included. This aircraft was modified by adding a pitch and yaw thrust-vectoring system. No significant problems occurred during the envelope expansion phase of the program.
Document ID
19930029276
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Regenie, Victoria
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Gatlin, Donald
(NASA Flight Research Center Edwards, CA, United States)
Kempel, Robert
(PRC, Inc. Edwards, CA, United States)
Matheny, Neil
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-4121
Report Number: AIAA PAPER 92-4121
Meeting Information
Meeting: AIAA, Biennial Flight Test Conference
Location: Hilton Head Island, SC
Country: United States
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: AIAA
Accession Number
93A13273
Distribution Limits
Public
Copyright
Other

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