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65 CSCL Administration Langley Research Administration Lewis Research aerodynamic aerodynamic characteristics Aeronautics and Space aerospace aircraft alloys analysis angle of attack applications atmosphere Author N68 axial boundary layer Brayton cycle calculations Calif CFSTI CFSTI HCS3 Cleveland coefficients computer program configuration cryogenic cylindrical density determine effects electrical electron equations evaluation experimental flow frequency fuel heat transfer hydrogen hypersonic inlet investigation Langley Research Center Langley Station launch vehicle Lewis Research Center liquid load lunar Mach number measurements method National Aeronautics nozzle nuclear obtained Ohio operation optimization orbit oxide parameters percent performance plasma predicted pressure propellant properties radiation range ratio reactor refs Contract Reynolds number rotor satellite simulated solar Space Administration Langley Space Administration Lewis spacecraft speed stress supersonic supersonic transport surface techniques temperature thermal trajectory trajectory optimization tube tungsten turbine turbulent V/STOL velocity vibration Washington Apr Washington May 1968 Washington NASA wind tunnel