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Effects of nose shape and fin geometry on static stability of a high-fineness-ratio sounding rocketNose shape and fin geometry effects on static stability of sounding rocket models in supersonic wind tunnel
Document ID
19680027037
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fuller, D. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1661
Accession Number
68N36509
Funding Number(s)
CONTRACT_GRANT: 124-07-05-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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