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Structural development of Topex/Poseidon satelliteThe Topex/Poseidon satellite's structural development approach adhered to more stringent requirements than previous efforts, since this spacecraft must withstand not only launch/flight loads but also those planned for the 'protoflight' vehicle's structural and environmental tests. There requirements encompassed conservatively estimated design loads, high safety factors, and extensive analytical simulations. The structural adequacy of the satellite was verified by means of a ground testing program to comply with both JPL institutional requirements and Arianespace requirements. Modal survey tests of the satellite have been successfully completed.
Document ID
19920050698
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lou, Michael C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Tsuha, Walter S.
(JPL Pasadena, CA, United States)
Larkin, Paul A.
(Fairchild Space Germantown, MD, United States)
Date Acquired
August 15, 2013
Publication Date
February 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-1224
Report Number: AIAA PAPER 92-1224
Accession Number
92A33322
Distribution Limits
Public
Copyright
Other

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