Thermodynamic analysis of dilute ternary systems. III - The Au-Cu-Sn system.
Heats of solution of Au and Cu in dilute Au-Cu-Sn alloys determined using liquid metal solution calorimeter, calculating self interaction coefficients
Pool, M. J.↗
SEARCH · Engineering Papers
Results for “Liquid Metal”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Magnetohydrodynamic rotation in an annulus
Liquid metal conductor confined between two concentric cylindrical electrodes
Cohen, I. M.↗
LM cathode thruster system Quarterly progress report, 4 Jan. 1969 - 4 Apr. 1970
Development of 20 cm liquid metal cathode thruster system
Bayless, J. R.↗
Research and advanced concepts
Electric arc deflected by transverse gas flow, and liquid metal MHD power conversion
Source record↗
A design study for a magnetohydrodynamic power system for a nuclear electric propelled unmanned spacecraft Final report, 26 May 1969 - 25 May 1970
Design of liquid metal magnetohydrodynamic power system for nuclear propulsion spacecraft
Source record↗
Two-fluid magnetohydrodynamic system and method for thermal-electric power conversion Patent
Thermoelectric power conversion by liquid metal flowing through magnetic field
Elliott, D. G.↗
Some topics in electrocatalysis
Liquid metal alloys surface composition and electronic structure roles in electrocatalysis evaluated by studying hydrogen-ion discharge reaction and electrical double layer
Butler, J. N.↗
Welding columbium-stainless bimetal tubing
Welding techniques for Nb-stainless steel bimetal tubing for liquid metal containment, determining structural integrity and bond interface condition after thermal cycling
Stoner, D. R.↗
Performance of a 20 cm LM cathode thruster system
Liquid metal /mercury/ cathode thrustor system for operation at reduced beam voltages, discussing design and performance
Bayless, J. R.↗
Reactor for nuclear extended range aircraft
High temperature liquid metal cooled nuclear reactor for military aircraft with long flight endurance and range
Orazio, F. D., Sr.↗
Investigation of the lithium-fluorine-hydrogen tripropellant system
Thermodynamic-kinetic analysis of fluorine/lithium/hydrogen tripropellant combustion efficiency, discussing liquid metal atomization, firings, facility and thrust chamber
Arbit, H. A.↗
High temperature cobalt-base alloy Patent
High temperature cobalt-base alloy resistant to corrosion by liquid metals and to sublimation in vacuum environment
Ashbrook, R. L.↗
Dynamical analysis of non-equilibrium forced convective boiling flows
Dynamical analysis of nonequilibrium, forced convective, boiling liquid metal flows
Pan, C. H. T.↗
Power system with heat pipe liquid coolant lines Patent
Electric power system with thermionic diodes and circulatory liquid metal coolant lines
Byrd, A. W.↗
Design of experiments as multiply telescoping sequences of blocks
Measuring elevated-temperature time-dependent corrosion effects of liquid metal on immersed structural materials
Holms, A. G.↗
Effect of velocity profile distortion in long dc electromagnetic flowmeters
Distorted velocity profile and electric potential distribution of long dc electromagnetic flowmeter for liquid metals
Chen, S.-M.↗
Design of experiments as 'multiply telescoping' sequences of blocks
Liquid metal elevated temperature time dependent corrosion effects on immersed structural materials, discussing blocked two level factorial experiment design for multiply telescoping sequences
Holms, A. G.↗
Fabrication and test of a space power boiler feed electromagnetic pump. 3: Endurance and final performance tests
A three-phase helical induction electromagnetic pump designed for the boiler feed pump of a potassium Rankine cycle space power system was developed and built. It was mounted in a liquid metal test loop and successfully tested over a range of potassium temperatures from 900 to 1400 F, flow rates from 0.75 to 4.85 lb/sec, developed pressures up to 340 psi, net positive suction head from 1 to 22 psi, and NaK coolant temperatures from 800 to 950 F. Maximum efficiency at design point conditions of 3.25 lb/sec flow rate, 240 psi developed head, 1000 F potassium inlet temperature, and 800 F NaK coolant inlet temperature was 16.3 percent. After the performance tests the pump was operated without any difficulty at design point for 10,000 hours, and then a limited number of repeat performance tests were made. There was no appreciable change in pump performance after 10,000 hours of operation. A supplementary series of tests using the quasi-square wave power output of a dc to three-phase ac inverter showed that the pump would operate without difficulty at a frequency as low as 25 Hz, with little loss in efficiency.
Powell, A. H.↗