By T. M. Flynn, B. W. Birmingham (auth.), K. D. Timmerhaus (eds.)
Invited Papers.- Cryogenics and nationwide Goals.- A evaluation of the potential for Liquid-Methane gasoline for Supersonic Transports.- Slush and Subcooled Propellants for Lunar and Interplanetary Missions.- Thermodynamic Properties.- Equilibrium Gas-Phase Compositions of Ethane and Ethylene in Binary combos with Helium and Neon less than 150°K and a Correlation for Deviations from the Geometric suggest Combining Rule.- The Kinetics of Adsorption of Methane and Nitrogen from Hydrogen Gas.- Benedict-Webb-Rubin Equation of country for Methane at Cryogenic Conditions.- a brand new Calorimeter for the exact selection of the Enthalpy of Pressurized Fluids all the way down to 160°R.- homes of Materials.- Simultaneous size of Young’s Modulus and Shear Modulus at Low Temperatures.- Tensile houses and Notch longevity of Groove Welds in Wrought and solid Aluminum Alloys at Cryogenic Temperatures.- Low-Temperature Mechanical houses of Welded and Brazed Copper.- Superconductivity.- A excessive box Magnet Combining Superconductors with Water-Cooled Conductors.- huge Superconducting Baseball Magnet.- trying out Composite Superconductor for the LRL Baseball Magnet.- temporary reaction and balance Limits of Superconducting Composite cord Following a Flux Jump.- Flux-Flow experiences and balance standards of Nb-Ti Strips.- The Transition to Current-Sharing in Composite Conductors.- balance of Internally Cooled Superconductors.- results of Nucleate Cooling Limits at the functionality of Small Ti-Nb Solenoids.- warmth Transfer.- Non-Boiling and movie Boiling warmth move to a Saturated bathtub of Liquid Helium.- Boiling warmth move and strain Drop of Liquid Helium-I lower than compelled circulate in a Helically Coiled Tube.- Nucleate Boiling warmth move from an Oscillating Sphere in Liquid Nitrogen.- A Miniature warmth Exchanger for Simultaneous Para-Orthohydrogen Conversion and warmth Transfer.- word on warmth Exchanger layout for Cryogenic Propellant Tanks.- A Compact Perforated-Plate warmth Exchanger.- Insulation.- Analytical versions for Airborne-Cryogenic-Insulation Thermal Performance.- overview of an Externally Insulated Spacecraft Dewar.- Experimental decision of Thermal lodging Coefficients.- Thermal Diffusivity of Powder Insulation.- Predictions of the complete Emissivity of Metals at Cryogenic Temperatures.- Radiative features of Cryodeposits for Room Temperature Black physique Radiation.- Fluid Dynamics.- Thermal Stratification in Closed Cryogenic Containers.- Approximate Criterion for Prediction of circulate Oscillations in Supercritical Fluid warmth Exchangers.- The interplay of regulate Valves with Oscillations Generated in a wide Water to Hydrogen warmth Exchanger.- Cavitation in Liquid Cryogens.- An research of the consequences of Spatial, Thermal, and pace Inhomogeneities on Two-Phase, unmarried part Cryogenic Choked Flow.- Two-Phase (Liquid-Vapor), Mass-Limiting movement with Hydrogen and Nitrogen.- Instrumentation.- Cryogenic circulation study Facility of the nationwide Bureau of Standards.- Prelaunch Slush Hydrogen Loading components Affecting Instrumentation and Control.- Use of Capacitance point Gauging for Prelaunch Loading of Slush Hydrogen.- growth on Cryogenic Thermocouples.- Fluid section and Temperature size with a unmarried Sensor.- lights in Cryogenic and Noncryogenic Fluids.- Refrigeration Systems.- An research of the Stirling-Cycle Refrigerator.- Steady-State Operation of the Idealized Vuilleumier Refrigerator.- Compact Cryogenic Thermal Regenerator Performance.- unfastened Displacer Refrigeration.- Dynamical results of the Rhombic force for Miniature Cooling Engines.- improvement of a pragmatic Thermodynamic Cycle for a Space-Borne Hydrogen Reliquefier.- A 3.6°K Reciprocating Refrigerator.- improvement of Novel gasoline Bearing Supported Cryogenic enlargement Turbines.- Miniature Cryogenic fridge Turboalternators.- keep an eye on method for Temperatures and Liquid point among 4.2° and 1°K.- Closed-Cycle fridges for Hydrogen Targets.- Cryogenic Systems.- Solidified Oxygen for inhaling Space.- Slush Hydrogen Pumping features utilizing a Centrifugal-Type Pump.- try out result of a Zero-Gravity Cryogenic section Separator.- Hydrogen Peroxide Motor Exhaust Heating to parts at Cryogenic Temperatures within the Vacuum of Space.- research of Propagation mess ups of versatile Linear formed fees at Cryogenic Temperatures.- The habit of average Liquid Hydrogen aim platforms less than Simulated Failure Modes.
Read or Download Advances in Cryogenic Engineering: Proceedings of the 1968 Cryogenic Engineering Conference Case Western Reserve University Cleveland, Ohio August 19–21, 1968 PDF
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Extra resources for Advances in Cryogenic Engineering: Proceedings of the 1968 Cryogenic Engineering Conference Case Western Reserve University Cleveland, Ohio August 19–21, 1968
Sindt, P. R. Ludtke, and D. B. Chelton, NBS Rept. 9265 (December, 1966). 20. D. E. Daney, P. R. Ludtke, C. F. Sindt, and D. B. Chelton, NBS Rept. 9701 (December, 1967). 21. N. E. Stanley, D. P. Hilgenberg, D. J. Hollweger, J. L. McDaniels, R. L. Rhoton, and J. S. Shaw, "Subcooled and Slush Hydrogen Properties, Systems Characteristics and Design Methods," McDonnell Rept. F65-76-941, Progress Rept. 004 (January-June, 1967). 22. D. H. Weitzel, C. F. Sindt, and D. E. 13, Plenum Press, New York (1968), p.
This suggested the use of the ionization potential I as a parameter for correlating the deviations from the Equilibrium Gas-Phase Compositions of Ethane and Ethylene in Binary Mixtures 39 combining rule. It is found that the value of k12 in equation (2) is best represented by (3) where v and c refer to the volatile and condensable components, respectively. The basic assumption is that the geometrie mean represents the maximum interaetion energy, and that k 12 is always positive. The ionization potentials employed in (3), exeept for Ar  and CH 4 [28J, can be taken from the Handbook oi Chemistry and Physics.
Psia Fig. 1. Heat absorption from initial state to venting of saturated gas. Studies show that the propellant heat input du ring long term storage missions generally exceeds 10 Btu/lb, which is substantially higher than the approximate 2 Btu/lb during ascent of current vehicles. The superior capability of slush and subcooled cryogens to absorb heat input can enhance space vehicle design and operations through: (a) increased storability for long term missions; (b) reduced tank insulation (quantity or quality); (c) reduced tank venting frequency; and (d) reduced tank size and operating pressure.