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Space station structural performance experimentA flight experiment that could be used to measure Space Station dynamics during and after its assembly is discussed. By integrating sensors into the structure to measure its ambient dynamic responses, it will provide some information as to how it behaves during its evolution. The objectives of the experiment are to define a series of experiments to measure the dynamic responses due to disturbances to establish the experiment scenarios, and to identify the locations of the instrumentation that can be integrated into the structure. Researchers have also defined the Space Station resources that are required so that they can be included in the Mission Requirements Data Base (MRDB). They used the 16-flight-assembly scenario that was recommended by Rockwell as the baseline.
Document ID
19910003111
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gates, Dick
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1990
Publication Information
Publication: NASA, Marshall Space Flight Center, Measurement and Characterization of the Acceleration Environment on Board the Space Station
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91N12424
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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