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Dynamics of towed deceleratorsTwo body mathematical model for flexible tow line- decelerator dynamical system
Document ID
19690010544
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Campbell, J. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1968
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-61528
Report Number: NASA-TM-X-61528
Accession Number
69N19898
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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