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Derivation of improved load transformation matrices for launchers-spacecraft coupled analysis, and direct computation of margins of safetyLoad and stress recovery from transient dynamic studies are improved upon using an extended acceleration vector in the modal acceleration technique applied to structural analysis. Extension of the normal LTM (load transformation matrices) stress recovery to automatically compute margins of safety is presented with an application to the Hubble space telescope.
Document ID
19900001761
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klein, M. (European Space Agency. European Space Research and Technology Center ESTEC, Noordwijk (Netherlands)., United States)
Reynolds, J. (British Aerospace Public Ltd. Co. Bristol, United Kingdom)
Ricks, E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Publication Information
Publication: ESA, Spacecraft Structures and Mechanical Testing
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N11077
Distribution Limits
Public
Copyright
Other
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