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Structural verification of the TOPEX/Poseidon satelliteThe prototype flight structural design and verification concept developed for TOPEX/Poseidon is presented. The structural configuration, design requirements, verification plan, analysis, and system level testing are described. The principal goal of the mission is to observe and measure ocean currents via radio altimetry, for enhanced knowledge of the interaction between the atmosphere and ocean.
Document ID
19920073108
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Larkin, Paul A.
(Fairchild Space Aviation Germantown, MD, United States)
Lou, Michael C.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 92-0304
Report Number: IAF PAPER 92-0304
Accession Number
92A55732
Distribution Limits
Public
Copyright
Other

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