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Historical overview of V/STOL aircraft technologyThe requirements for satisfactory characteristics in several key technology areas are discussed and a review is made of various V/STOL aircraft for the purpose of assessing the success or failure of each design in meeting design requirements. Special operating techniques were developed to help circumvent deficiencies. For the most part performance and handling qualities limitations restricted operational evaluations. Flight operations emphasized the need for good STOL performance, good handling qualities, and stability and control augmentation. The majority of aircraft suffered adverse ground effects.
Document ID
19810010574
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Anderson, S. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81280
A-8511
Accession Number
81N19100
Funding Number(s)
PROJECT: RTOP 505-42-71
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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