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Powered-lift technology on the thresholdA design configuration study and comparative performance evaluation is presented for current and planned V/STOL military aircraft and their powerplant and control systems, with a view to the effect of the operational capabilities uniquely furnished by such aircraft for battlefield tactics. Attention is given to V/STOL naval aircraft and the carrier or ship's deck conditions under which they must be able to operate. Thrust-vectoring and tilt rotor configurations are the most prominent among successful experimental and operational aircraft of this type; cargo aircraft have most often incorporated short/rough airfield operation capabilities rather than full VTOL. A major development thrust has been mounted for a supersonic short takeoff/vertical landing aircraft.
Document ID
19860029507
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Deckert, W. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Franklin, J. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1985
Publication Information
Publication: Aerospace America
Volume: 23
ISSN: 0740-722X
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ISSN: 0740-722X
Accession Number
86A14245
Distribution Limits
Public
Copyright
Other

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