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THE INFLUENCE OF SHAPE ON AERODYNAMIC DAMPING OF OSCILLATORY MOTION DURING PLANET ATMOSPHERE ENTRY AND MEASUREMENT OF PITCH DAMPING AT LARGE OSCILLATION AMPLITUDESReentry vehicle shape effects on the accuracy and angle-of-attack amplitude and wind tunnel methods for measuring pitch damping
Document ID
19630027341
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Babineaux, T. L.
Brayshaw, J. M., Jr.
Dayman, B., Jr.
Nelson, D. A.
Date Acquired
August 1, 2013
Publication Date
January 1, 1963
Subject Category
Aircraft
Accession Number
63A23400
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT REENTRY
PLANETARY ENTRY
REENTRY VEHICLE

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