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Optimization of Weight Including Damage Scenarios, Phase I
Completed
Description
M4 Engineering proposes to develop a method of incorporating several analyses into one process and then optimizing the structure. This method will allow for significant weight savings of structural compoents by incorporating analyses for damage tolerance, and durability in the design phase. Damage tolerance analyses, especially, have been difficult to iterate on since it has been time consuming to create models of each damage condition. The proposed method will be a highly efficient and useful method in reducing weight of structures.
Details
| Technology area | Flight Vehicle Systems > Aeroscience > Aeroelasticity |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Glenn Research Center, Cleveland, OH |
| Start date | 2008-01-18 |
| End date | 2008-07-21 |
Project contacts
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How to get involved
This is a mature technology (TRL 7+) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.
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