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    Mach number and Reynolds number effect on orbiter/tank interference heating. (1973)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: Analysis of the variations in orbiter/tank interference heating rates in the Space Shuttle configuration at M numbers up to 19 and Re numbers down to 250,000. Experimental data on heat transfer rate distribution in the tank and on orbiter-induced interference heat transfer factors in the tank are included in diagrams. The data suggest that the primary effect of interference can be a fully developed turbulent boundary layer.
    Keywords: SPACE VEHICLES
    Type: Journal of Spacecraft and Rockets; 10; Aug. 197
    Format: text
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