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A wind tunnel free flight testing technique for nonplanar motion of spinning models.Wind tunnel free-flight testing of reentry vehicle dynamics, noting capability for simultaneous two- dimensional viewing of model trajectories
Document ID
19660061364
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Holway, H. P.
Prislin, R. H.
Date Acquired
August 3, 2013
Publication Date
September 1, 1966
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 66-774
Report Number: AIAA PAPER 66-774
Accession Number
66A40654
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY ANALYSIS
FREE FLIGHT TEST APPARATUS
DYNAMIC STABILITY
WIND TUNNEL APPARATUS
REENTRY VEHICLE

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