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 abstract in SAE -- J v 69 n 7 July 1961 p 96-8)
Thermal radiation as high temperature energy transport mechanism within solids
SAE -- Paper
SAE Meeting ; 1961 Nozzles
1961
10 pages
Aufsatz (Konferenz)
Englisch
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