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Sea based support aircraft alternativesMulti-mission, CTOL, STOL and V/STOL aircraft concepts were sized for the Navy ASW/ASUW missions and comparatively evaluated. Initially, technology levels in the areas of lift, control systems, propulsion, advanced materials and avionics were established for the early 1990's. The aircraft were compared to determine the impact of multi-mission requirements, operational considerations, chiefly takeoff mode, as well as the technology advancements. Results presented include performance envelopes, weight statements, growth factors, impact of technology on weight reduction and the impact of design constraints.
Document ID
19820035682
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Priestley, R. T.
Yackle, A. R.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
August 10, 2013
Publication Date
December 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 81-2649
Report Number: AIAA PAPER 81-2649
Meeting Information
Meeting: V/STOL Conference
Location: Palo Alto, CA
Start Date: December 7, 1981
End Date: December 9, 1981
Sponsors: American Institute of Aeronautics and Astronautics and NASA Ames Research Center
Accession Number
82A19217
Distribution Limits
Public
Copyright
Other

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