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A Multi-Physics CFD Toolkit for Reentry Flows, Phase I
Completed
Description
AeroSoft proposes to develop a full featured CFD toolkit for analysis of the aerothermal environment and its effect on space vehicles. In Phase I, AeroSoft proposes to implement multi-component ablation along with material response into AeroSoft's structured and unstructured CFD solver GASP. In Phase I, GASP's internal thermal solver will be augmented to include the effects of ablation. In Phase II, AeroSoft proposes to implement radiation heat flux and radiation transport into GASP.
Details
| Technology area | Entry, Descent, and Landing > Vehicle Systems > Integrated Modeling and Simulation for EDL |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Langley Research Center, Hampton, VA |
| Start date | 2008-01-25 |
| End date | 2008-07-24 |
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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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