Evaluation of radiative transport as means for removing heat from rocket nozzle walls; mechanisms contributing to ordinary thermal conductivity of metals and dielectrics and factors limiting conductivity; radiative transport and ordinary conductivity characteristics of solids are compared; analysis of rocket nozzle design illustrating advantages of using radiative transport within solids to extract heat from nozzle wall. (See also SAE -- Paper 354A for meeting Apr 4-7 1961 10 p)
Thermal radiation as high temperature energy transport mechanism within solids
SAE -- J
Society of Automotive Engineers -- Journal ; 69 , n 7
1961
3 pages
Aufsatz (Zeitschrift)
Englisch
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