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Free flight simulated on ground with the Apollo Saturn V space vehicle.Hydraulic support system for free flight simulation with Saturn V-Apollo vehicle, discussing stability requirements, upper bounds of system design, conversion from nonlinear to linear model, etc
Document ID
19670059067
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Von Pragenau, G. L.
Date Acquired
August 3, 2013
Publication Date
September 1, 1967
Publication Information
Publication: /AIAA/JACC GUIDANCE AND CONTROL CONFERENCE
Subject Category
Facilities, Research, And Support
Accession Number
67A37796
Funding Number(s)
CONTRACT_GRANT: NAS8-11903
Distribution Limits
Public
Copyright
Other
Keywords
VIBRATION TESTING
BENDING THEORY
SATURN V LAUNCH VEHICLE
HYDRAULIC SYSTEM
STABILITY AND CONTROL

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