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Space shuttle: Effect of cruise engine nacelle arrangement and tail size on static stability and control effectivenessLow speed wind tunnel tests of straight wing and delta wing configuration space shuttle booster models
Document ID
19710025634
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zombek, Z. (Chrysler Corp. New Orleans, LA, United States)
Goldberg, W. (Chrysler Corp. New Orleans, LA, United States)
Rausch, J. (Chrysler Corp. New Orleans, LA, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1970
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-103162
DMS-DR-1039
DRL-184-58
Report Number: NASA-CR-103162
Report Number: DMS-DR-1039
Report Number: DRL-184-58
Accession Number
71N35110
Funding Number(s)
CONTRACT_GRANT: NAS8-4016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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