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Space shuttle: Effects of horizontal tail geometry and position on longitudinal stability of model S-5, NASA/MSC 0.01875 space orbiter shuttleLow speed wind tunnel test on effects of horizontal tail geometry on longitudinal stability of orbiter shuttle
Document ID
19710025608
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pope, H. A. (Chrysler Corp. New Orleans, LA, United States)
Date Acquired
August 6, 2013
Publication Date
March 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
DMS-DR-1073
NASA-CR-119858
Report Number: DMS-DR-1073
Report Number: NASA-CR-119858
Accession Number
71N35084
Funding Number(s)
CONTRACT_GRANT: NAS8-4016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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