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INVESTIGATION OF THE LOW-SUBSONIC STABILITY AND CONTROL CHARACTERISTICS OF A 0.34 -SCALE FREE-FLYING MODEL OF A MODIFIED HALF-CONE REENTRY VEHICLELow subsonic stability and control of a 0.34-scale free flying model of a half cone reentry vehicle
Document ID
19630004806
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hassell, J. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Ware, G. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1962
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-665
Report Number: NASA-TM-X-665
Accession Number
63N14682
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPACECRAFT MODEL
FREE FLIGHT
REENTRY VEHICLE
HALF-CONE
STABILITY AND CONTROL

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