Gas core reactors for MHD power systems
Gas core reactors and MHD generator to solve problems of growing demand for electric power without thermal pollution
Engineering topics
Publications and source records attributed to Williams, J. R..
Gas core reactors and MHD generator to solve problems of growing demand for electric power without thermal pollution
Optical surfaces contamination analysis by holographic interferometry, using fringe patterns for contaminant film thickness and uniformity
Experimental investigation and measurement of the radiant heat attenuation of an aerosol which may serve as a gas core nuclear-rocket propellant. The experiment uses a tungsten-hydrogen aerosol heated to temperatures as high as 2500 K under pressures up to 115 atmospheres. The hydrogen aerosol is produced by dispersion of submicron-sized particles of tungsten in hydrogen gas. A narrow beam of broad spectrum (visible and ultraviolet) light is passed through it with the attenuation being measured as a function of wavelength. Other aerosol characteristics examined include the nature and extent of chemical reactions between the seed material and the hydrogen and the degree of dispersion of the seed material obtained before and after heating. Chemical equilibrium calculations and vapor pressure data for the refractory metals indicate that tungsten is a prime candidate for the seed material in the gas core nuclear rocket.
The differential scattering parameter has been measured for 0.04-micron tungsten particles in hydrogen and nitrogen at temperatures to 1080 K. The differential scattering parameter has also been measured for 0.1 micron tungsten, three types of carbon particles, and fly ash in nitrogen at temperatures to 1000 K. The 0.04 micron tungsten shows a temperature dependent total scattering parameter varying from around 4000 sq cm per g at room temperature to 7000 sq cm per g at 1088 K. The temperatures over which data were obtained are not high enough to confirm the temperature dependence of the total scattering parameter of tungsten.
Seeded argon-hydrogen plasmas have been produced at Georgia Tech in order to experimentally measure composition, temperature, radiant heat output and opacity. The plasma, seeded with submicron tungsten particles, simulates the propellant of a gaseous core nuclear rocket. These measurements are needed to predict the dynamic behavior of the operating gas core reactor. The temperature range in which the seed has vaporized but the hydrogen itself has not yet become opaque is known as the seed-hydrogen opacity window. Preliminary opacity data in this temperature range will be presented.
Technique for monitoring deposition of films on surfaces, in place on a real-time basis, reads both the thickness and the uniformity of the deposited film. Holograms are produced from both reflected and transmitted light on one plate.
Device for nondestructive testing of soldered joints correlates stress with load to predict printed circuit board lifetime.
Extinction parameters of submicron carbon, tungsten and Si particles in hydrogen measured at various temperatures, discussing scattering amplitude functions and Monte Carlo calculations
Abstract operator represented for linear, homogeneous system as Lie group exhibiting metrics and conservation laws
Radiant heat transfer properties of particle seeded gases, including absorption and scattering characteristics of carbon, silicon, and tungsten
Extinction parameters of hydrogen aerosols at high temperatures
Physical properties of Martian atmosphere using solar occultation seen from artificial satellite
Diffusion and ion pump vacuum systems using ionic and kinetic methods of gas evacuation
Critical water depth required for hydroplaning
Space manufacturing operations program, discussing zero gravity effect during earth orbit flight, Apollo Applications Program Orbital Workshop Flight 2, etc
Correlation of lunar radii estimates obtained from earth based photographic study and lunar orbiter gravitational field coefficient measures
Seeded H thermal radiation absorptive properties evaluated for propellant temperatures in nuclear rockets as function of temperature
Continuum bursty emission from Jupiter at 18 MHz observed using interferometer