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Analysis of flow separation effects on the dynamics of a large space boosterFlow separation effect on large space booster - saturn i /sa-1/ launch vehicle
Document ID
19640016339
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ericsson, L.-E. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Reding, J. P. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 2, 2013
Publication Date
July 2, 1964
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER-64-482
Report Number: AIAA PAPER-64-482
Accession Number
64N26253
Funding Number(s)
CONTRACT_GRANT: NAS8-5338
Distribution Limits
Public
Copyright
Other
Keywords
FLOW SEPARATION

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