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Carbon-phenolic ablative thermal protection material for atmospheric reentry relies on the release and outflow of pyrolysis gas in the material. This results in a pressure increase in the material sample, for which little experimental data exists. We measure this internal pressure during ablation experiments and study its effect on the ejection of solid particles or fragmentation of the material.

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This page is a summary of: Experimental Investigation of Pyrolysis Pressure in Ablators and Its Effect on Spallation, Journal of Spacecraft and Rockets, August 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a36411.
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