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Multi-Scale Sizing of Lightweight Multifunctional Spacecraft Structural ComponentsThis document is the final report for the project entitled, "Multi-Scale Sizing of Lightweight Multifunctional Spacecraft Structural Components," funded under the NRA entitled "Cross-Enterprise Technology Development Program" issued by the NASA Office of Space Science in 2000. The project was funded in 2001, and spanned a four year period from March, 2001 to February, 2005. Through enhancements to and synthesis of unique, state of the art structural mechanics and micromechanics analysis software, a new multi-scale tool has been developed that enables design, analysis, and sizing of advance lightweight composite and smart materials and structures from the full vehicle, to the stiffened structure, to the micro (fiber and matrix) scales. The new software tool has broad, cross-cutting value to current and future NASA missions that will rely on advanced composite and smart materials and structures.
Document ID
20050185537
Acquisition Source
Headquarters
Document Type
Contractor or Grantee Report
Authors
Bednarcyk, Brett A.
(Ohio Aerospace Inst. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Spacecraft Design, Testing And Performance
Funding Number(s)
CONTRACT_GRANT: NCC3-878
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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