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Record Nr. |
UNINA9910716019603321 |
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Autore |
Schacht Ralph L. |
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Titolo |
Effective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings / / by Ralph L. Schacht, Harold G. Price, Jr., and Richard J. Quentmeyer |
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Pubbl/distr/stampa |
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Washington, D.C. : , : National Aeronautics and Space Administration, , November 1972 |
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Descrizione fisica |
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1 online resource (41 pages) : illustrations |
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Collana |
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Soggetti |
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Rocket firing |
Aeronautics |
Coatings - Thermal properties - Testing |
Heat - Transmission |
Composite materials - Effect of temperature on - Testing |
Rockets (Aeronautics) - Nozzles |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Nota di bibliografia |
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Includes bibliographical references (page 18). |
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Sommario/riassunto |
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An experimental investigation was conducted to determine the effective conductivities of four plasma-arc-sprayed, metal-ceramic gradated coatings on hydrogen-oxygen thrust chambers. The effective thermal conductivities were not a function of pressure or oxidant-to-fuel ratio. The various materials that made up these composites do not seem to affect the thermal conductivity values as much as the differences in the thermal conductivities of the parent materials would lead one to expect. Contact resistance evolving from the spraying process seems to be the controlling factor. The thermal conductivities of all the composites tested fell in the range of 0.75 to 7.5 watts per meter kelvin. |
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