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The aeroelastic characteristics of the Saturn-IB SA-201 launch vehicleAerodynamic damping determined as function of static load distribution for Saturn IB SA-201 VEHICLE from subsonic to supersonic speeds
Document ID
19660010784
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jecmen, D. M. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
August 1, 1965
Subject Category
Space Vehicles
Report/Patent Number
M-37-65-2
NASA-CR-71024
Report Number: M-37-65-2
Report Number: NASA-CR-71024
Accession Number
66N20073
Funding Number(s)
CONTRACT_GRANT: NAS8-11238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC SPEED
SUBSONIC SPEED
STATIC LOADING
SATURN IB LAUNCH VEHICLE
AERODYNAMIC CHARACTERISTICS
DAMPING

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