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NASA NTRS · 19890013300

Thrust Chamber Thermal Barrier Coating Techniques

Richard J Quentmeyer
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Abstract

Methods for applying thermal barrier coatings to the hot-gas side wall of rocket thrust chambers in order to significantly reduce the heat transfer in high heat flux regions has been the focus of technology efforts for many years. A successful technique developed by NASA-Lewis that starts with the coating on a mandrel and then builds the thrust chamber around it by electroforming appropriate materials is described. This results in a smooth coating with exceptional adherence, as was demonstrated in hot fire rig tests. The low cycle fatigue life of chambers with coatings applied in this manner was increased dramatically compared to uncoated chambers.

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BibTeXRIS

Richard J Quentmeyer. 1989-03-01. Thrust Chamber Thermal Barrier Coating Techniques. https://ntrs.nasa.gov/citations/19890013300

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