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Computation of structural modes of a rollout array spacecraft for attitude control studyStructural modes required to determine interaction between attitude control system and flexible deployed solar electric spacecraft
Document ID
19710015679
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Weiner, E. O. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-118327
JPL-TM-33-476
Report Number: NASA-CR-118327
Report Number: JPL-TM-33-476
Accession Number
71N25155
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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