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Low-speed tests of an all-flexible parawing for landing a lifting-body spacecraftWind tunnel and flight tests to determine aerodynamic characteristics and rigging control of flexible parawing for lifting body spacecraft
Document ID
19670019428
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bugg, F. M. (NASA Langley Research Center Hampton, VA, United States)
Sleeman, W. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4010
Report Number: NASA-TN-D-4010
Accession Number
67N28757
Funding Number(s)
CONTRACT_GRANT: 124-07-03-22-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
FLEXIBLE WING
LIFTING BODY
PARAWING

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