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V/STOL Capability by Modifying CTOL Aircraft

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kuhn, R. E., author.
Conference Name:
Aerospace Congress & Exposition (1980-10-13 : Los Angeles, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1980
Summary:
The increasing cost and vulnerability of conventional airbases and aircraft carriers places increasing emphasis on the continuing application of V/STOL technology. This paper reviews the status of V/STOL technology. The helicopter and the Harrier have proven themselves and the improved AV-8B is being developed.This paper examines the possibilities of modifying CTOL aircraft to give them V/STOL capability to fill two other aircraft/mission areas; an air superiority V/STOL and a V/STOL type to fill the ASW, AEW, and missileer roles. Recommendations are made for a program to investigate such modifications of existing CTOL aircraft now used in these roles so that the application of V/STOL capability to these missions can be explored and evaluated. Other recommendations are made with respect to the need for engine out hover capability, the use of Short Take-Off and Vertical Landing (STO-VL) capability and the need for special V/STOL engine ratings
Notes:
Vendor supplied data
Publisher Number:
801179
Access Restriction:
Restricted for use by site license

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