The requirements for tactical fighter aircraft in the early nineties will call for improved maneuverability from current fighters, as well as shorter takeoff and landing distances, reduced radar cross-sections and IR signatures, and supersonic persistence. Also, the cost of procurement, operation and maintenance of the engine (LCC) will be a significant parameter in determining the type and performance of the next fighter engine. Each of the above requirements has an effect on the engine cycle to be chosen for the next fighter engine. The sum of these effects should result in a specific engine cycle which best answers all of the aircraft needs, but the effects of these requirements tend toward diverse cycles. This paper addresses these issues and presents a comparison of cycles that meet the anticipated requirements for tactical fighter aircraft in the early nineties. The paper also compares the usage of such aircraft in peacetime training to the design mission in combat.
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ASME 1982 International Gas Turbine Conference and Exhibit
April 18–22, 1982
London, England
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7957-3
PROCEEDINGS PAPER
Cycle Considerations for Tactical Fighters in the Early 1990’s
H. D. Snyder
H. D. Snyder
Pratt & Whitney Aircraft, West Palm Beach, FL
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H. D. Snyder
Pratt & Whitney Aircraft, West Palm Beach, FL
Paper No:
82-GT-259, V002T02A015; 5 pages
Published Online:
April 15, 2015
Citation
Snyder, HD. "Cycle Considerations for Tactical Fighters in the Early 1990’s." Proceedings of the ASME 1982 International Gas Turbine Conference and Exhibit. Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery. London, England. April 18–22, 1982. V002T02A015. ASME. https://doi.org/10.1115/82-GT-259
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