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Space Station Freedom solar dynamic modules structural modelling and analysisIn support of the Space Station Freedom (SSF) Solar Dynamic Power Module effort, structural design studies were performed to investigate issues related to the design of the power module, its pointing capabilities, and the integration of the module into the SSF infrastructure. Of particular concern from a structural viewpoint are the dynamics of the power module, the impact of the power module on the Space Station dynamics and controls, and the required control effort for obtaining the specified Solar Dynamic Power Module pointing accuracy. Structural analyses were performed to determine the structural dynamics attributes of both the existing and the proposed structural dynamics module designs. The objectives of these analyses were to generate validated Solar Dynamic Power Module NASTRAN finite element models, combine Space Station and power module models into integrated system models, perform finite element modal analyses to assess the effect of the relocations of the power module center of mass, and provide modal data to controls designers for control systems design.
Document ID
19920006187
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lawrence, Charles
(NASA Lewis Research Center Cleveland, OH, United States)
Morris, Ron
(Sverdrup Technology, Inc., Brook Park OH., United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:104506
E-6367
NASA-TM-104506
Report Number: NAS 1.15:104506
Report Number: E-6367
Report Number: NASA-TM-104506
Accession Number
92N15405
Funding Number(s)
PROJECT: RTOP 505-63-1B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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