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Results of a free-flight test to determine the performance characteristics of a towed, conical deceleratorDrag and stability characteristics of towed, conical decelerator
Document ID
19690029213
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Usry, J. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1969
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1833
Report Number: NASA-TM-X-1833
Accession Number
69N38598
Funding Number(s)
CONTRACT_GRANT: 124-07-03-05-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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