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Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7
Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7
By Don E. Avery
Sensors for a system to control the liquid flow into an evaporative cold plate of a two-phase heat transport system for large spacecraft
Sensors for a system to control the liquid flow into an evaporative cold plate of a two-phase heat transport system for large spacecraft
By A. A. M. Delil