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  • 1
    facet.materialart.
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    Plasma tests of sprayed coatings for rocket thrust chambers (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Several plasma-sprayed coating systems were evaluated for structural stability in hydrogen plasma and in oxygen plasma mixed with hydrogen plasma. The principal test heat flux was 15 Btu per inch squared seconds. The system consisted of a number of thin 0.002 to 0.020 in. layers of metal oxides and/or metals. The principal materials included are molybdenum nichrome, alumina, and zirconia. The study identifies important factors in coating system fabrication and describes the durability of the coating systems in the test environments. Values of effective thermal conductivity for some of the systems are indicated.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-TM-X-3072 , E-7877
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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