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NASA NTRS · 20200000628

Microscale Analysis of Spacecraft Heat Shields

Abstract

Imagine entering Earth’s atmosphere after returning from the outer solar system. A heat shield less than 2 inches thick protects you from temperatures up to 2,900° Celsius (5,252° Fahrenheit). Such conditions were experienced by NASA’s Stardust capsule during reentry in 2006. The only materials capable of providing the necessary protection are composites with complex microstructures. Evaluating these materials is difficult, requiring precise knowledge of their properties. To this end, NASA scientists are developing research codes to compute material properties and simulate ablation at the microscale using agency supercomputers. Utilizing these tools, along with experiments, researchers are working to push the limits of spaceflight, allowing for greater flexibility in future space missions.

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BibTeXRIS

Thornton, John M., Semeraro, Federico, Visser, Sander J., Borner, Arnaud, Ferguson, Joseph C., Panerai, Francesco, Mansour, Nagi N.. 2019-11-17. Microscale Analysis of Spacecraft Heat Shields. https://ntrs.nasa.gov/citations/20200000628

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