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The aeroelastic characteristics of the Saturn IB SA-203 launch vehicleAeroelastic properties, and effects of boundary layer-terminal shock wave interaction on Saturn IB SA-203 launch vehicle
Document ID
19660022850
Document Type
Contractor Report (CR)
Authors
Ericsson, L. E. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
French, N. J. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Subject Category
SPACE VEHICLES
Report/Patent Number
NASA-CR-76563
M-37-66-2
Funding Number(s)
CONTRACT_GRANT: NAS8-11238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AEROELASTICITY
SATURN LAUNCH VEHICLE
SHOCK WAVE INTERACTION

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NameType 19660022850.pdf STI