What people are saying - Write a review
We haven't found any reviews in the usual places.
TEMPERATURE CONTROL FOR LUNAR VEHICLES
RADIATION HEAT TRANSFER FROM EXTENDED
23 other sections not shown
Other editions - View all
ammonia analysis analyzed approximately available energy Brayton cycle Btu/hr Btu/lb Carnot cycle cent Combining Eqs compressor computed configuration factor cooling curves data of Fig decomposition determined differential direct cycle duct dZjdco effectiveness emissivity engine enthalpy Entropy environment equal equations evaluated extended surfaces fin length fluid cycle fluid parameter free space Freon gases heat exchanger heat of solution heat radiated heat rejected heat transfer heat-transfer higher hydrazine hydrogen increase latent heat lithium hydride lunar mercury Minimum radiator area mixture monopropellants moon nondimensional obtained optimum-weight plotted powerplant prime mover problem profile number propellant Rankine cycle reduced refrigeration root thickness rubidium saturated vapor selected shown in Fig solar space vehicle specific heat storage Substituting superheat temperature control theoretical profile thermal efficiency triangular fin tube turbine efficiency Turbine inlet temperature vapor passageway vapor pressure vertical surface wall temperature weight zero