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Continuous and discrete RAE structural models.Three dimensional coupled flexural and attitude dynamics of libration-damped cruciform gravity gradient satellite, discussing effects of orbital eccentricity, solar radiation pressure, etc
Document ID
19690061222
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Farrell, J. L.
Newton, J. K.
Date Acquired
August 5, 2013
Publication Date
April 1, 1969
Subject Category
Space Vehicles
Report/Patent Number
AAS PAPER 68-126
Meeting Information
Meeting: AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ASTRODYNAMICS SPECIALIST CONFERENCE
Location: JACKSON, WYO.
Start Date: September 3, 1968
End Date: September 5, 1968
Sponsors: AMERICAN ASTRONAUTICAL SOCIETY AND AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A39211
Funding Number(s)
CONTRACT_GRANT: NAS5-9753-15
CONTRACT_GRANT: NAS5-9753-10
Distribution Limits
Public
Copyright
Other

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