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Total systems design analysis of high performance structuresDesigner-control parameters were identified at interdiscipline interfaces to optimize structural systems performance and downstream development and operations with reliability and least life-cycle cost. Interface tasks and iterations are tracked through a matrix of performance disciplines integration versus manufacturing, verification, and operations interactions for a total system design analysis. Performance integration tasks include shapes, sizes, environments, and materials. Integrity integrating tasks are reliability and recurring structural costs. Significant interface designer control parameters were noted as shapes, dimensions, probability range factors, and cost. Structural failure concept is presented, and first-order reliability and deterministic methods, benefits, and limitations are discussed. A deterministic reliability technique combining benefits of both is proposed for static structures which is also timely and economically verifiable. Though launch vehicle environments were primarily considered, the system design process is applicable to any surface system using its own unique filed environments.
Document ID
19940015668
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Verderaime, V.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1993
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TP-3432
NAS 1.60:3432
M-733
Report Number: NASA-TP-3432
Report Number: NAS 1.60:3432
Report Number: M-733
Accession Number
94N20141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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