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Relative influence of atmospheric properties on launch vehicle design.Atmospheric density, winds and turbulence relative influence on Saturn V vehicle control system and structural bending moment response during Atlantic Missile Range ascent flight
Document ID
19670040643
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bieber, R. E.
Date Acquired
August 3, 2013
Publication Date
February 1, 1967
Publication Information
Publication: /AMERICAN METEOROLOGICAL SOCIETY
Subject Category
Space Vehicles
Report/Patent Number
AIAA PAPER 66-341
Report Number: AIAA PAPER 66-341
Accession Number
67A19372
Funding Number(s)
CONTRACT_GRANT: NAS8-11453
Distribution Limits
Public
Copyright
Other
Keywords
WIND EFFECT
DYNAMIC RESPONSE
ATMOSPHERIC CONDITION EFFECT
ASCENT TRAJECTORY
SATURN V LAUNCH VEHICLE
BENDING MOMENT
TURBULENCE EFFECT

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