NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The ultralight sailplaneAs presently envisioned, the ultralight sailplane is intermediate in size, cost and performance between current hang gliders and the lower end of the traditional sailplane spectrum. In the design of an ultralight sailplane, safety, low cost, and operational simplicity were emphasized at the expense of absolute performance. An overview of the design requirements for an ultralight sailplane is presented. It was concluded that by a judicious combination of the technologies of hang gliding, human powered flight, conventional soaring and motor gliding, an operationally and economically viable class of ultralight, self-launching sailplanes can be developed.
Document ID
19790018909
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcmasters, J. H.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Publication Information
Publication: NASA. Langley Res. Center Sci. and Technol. of Low Speed and Motorless Flight
Subject Category
Aircraft Design, Testing And Performance
Accession Number
79N27080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available