Considerable effort is now under way to develop technologies for enhancing fighter maneuvering limits. This has in part been motivated by the capabilities of advanced air-to-air missiles. One approach to enhanced combat effectiveness involves flight envelope expansion and improved controllability via engine thrust-vectoring and thrust-reversing. The complexity of fighter combat, however, makes it difficult to perform engineering analyses for assessing potential technological enhancements and risks. This paper describes a digital simulation that has been used to identify benefits associated with improved maneuverability. The Navy/Grumman F-14 aircraft provides the flight characteristics database. Combat tactics are developed as part of the solution process and are based solely on characteristics of the combatants and weapons employed. Head-on and codirectional neutral start combat engagements are used to illustrate study results.
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January 1994
Research Papers
Thrust Vectoring/Reversing Tactics in Air-to-Air Combat
C. W. Boppe,
C. W. Boppe
Grumman Corporation, Bethpage, NY 11714
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R. P. Martorella
R. P. Martorella
Grumman Corporation, Bethpage, NY 11714
Search for other works by this author on:
C. W. Boppe
Grumman Corporation, Bethpage, NY 11714
R. P. Martorella
Grumman Corporation, Bethpage, NY 11714
J. Eng. Gas Turbines Power. Jan 1994, 116(1): 124-132 (9 pages)
Published Online: January 1, 1994
Article history
Received:
March 13, 1992
Online:
April 24, 2008
Citation
Boppe, C. W., and Martorella, R. P. (January 1, 1994). "Thrust Vectoring/Reversing Tactics in Air-to-Air Combat." ASME. J. Eng. Gas Turbines Power. January 1994; 116(1): 124–132. https://doi.org/10.1115/1.2906781
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