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Dive into the research topics where Edwin C. Ethridge is active.

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Featured researches published by Edwin C. Ethridge.


Annals of the New York Academy of Sciences | 2004

Effects of Gravity on ZBLAN Glass Crystallization

Dennis S. Tucker; Edwin C. Ethridge; Guy A. Smith; Gary L. Workman

Abstract: The effects of gravity on the crystallization of ZrF4‐BaF2‐LaF3‐AlF3‐NaF glasses have been studied using the NASA KC‐135 and a sounding rocket. Fibers and cylinders of ZBLAN glass were heated to the crystallization temperature in unit and reduced gravity. When processed in unit gravity the glass crystallized, but when processed in reduced gravity, crystallization was suppressed. A possible explanation involving shear thinning is presented to explain these results.


Space | 1998

Processing Glass Fiber from Moon/Mars Resources

Dennis S. Tucker; Edwin C. Ethridge

Processing of Lunar/Mars raw materials into usable structural and thermal components for use on a Lunar/Mars base will be essential for human habitation. One such component will be glass fiber which can be used in a number of applications. Glass fiber has been produced from two lunar soil simulants. These two materials simulate lunar mare and lunar highlands soil compositions. Short fibers containing recrystallized areas were produced from the as-received simulants. Doping the highland simulant with 8 weight percent boria yielded a material which could be spun continuously. The effects of lunar gravity on glass fiber formation were studied utilizing NASAs KC 135 aircraft. Gravity was found to play a role in crystallization and final fiber diameter.


Advances in Space Research | 1999

Utilization of low gravity environment for measuring the viscosity of highly viscous liquids

Basil N. Antar; Edwin C. Ethridge; D. Maxwell

Abstract The method of drop coalescence is utilized for determining the viscosity of highly undercooled liquids. Low gravity environment is necessary in order to avoid problems connected with droplet deformation due other body forces that are present under terrestrial conditions. The drop coalescence method is preferred over the drop oscillation technique since the latter method can only be applied for liquids with vanishingly small viscosities. The technique developed relies on both the highly accurate solution of the equations of motion for fluid flows as well as on data from experiments conducted in near zero gravity environment. Results are presented for method validation experiments performed recently on board the NASA/KC-135 aircraft. These experiments gave excellent results which will be discussed together with plans for implementing the method in a shuttle flight experiment.


SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM-STAIF 2007: 11th Conf Thermophys.Applic.in Micrograv.; 24th Symp Space Nucl.Pwr.Propulsion; 5th Conf Hum/Robotic Techn & Vision Space Explor.; 5th Symp Space Coloniz.; 4th Symp New Frontrs & Future Con | 2007

Microwave Extraction of Water from Lunar Regolith Simulant

Edwin C. Ethridge; William F. Kaukler

Nearly a decade ago the DOD Clementine lunar orbital mission obtained data indicating that the permanently shaded regions at the lunar poles may have permanently frozen water in the lunar soil or ‘permafrost’. Currently a Lunar Lander Exploration Program is expected to land at the lunar pole to determine if water is present. The detection of water from the permafrost is an important goal for NASA. Extraction of water from lunar permafrost would be a valuable In‐Situ Resource for Utilization (ISRU) in human life support and as a fuel. The use of microwave processing could permit the extraction of water without the need to dig, drill, or excavate the lunar surface. Microwave heating of regolith is potentially faster and more efficient than any other heating methods due to the very low thermal conductivity of the lunar regolith. Also, microwaves can penetrate into the soil permitting water removal from deep below the lunar surface. A cryogenic vacuum test facility was developed for evaluating the use of micr...


49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition | 2011

Microwave Processing of Planetary Surfaces for the Extraction of Volatiles

Edwin C. Ethridge; William F. Kaukler

In-Situ Resource Utilization will be necessary for sustained exploration of space. Volatiles are present in planetary soils, but water by far has the most potential for effective utilization. The presence of water at the lunar poles, Mars, and possibly on Phobos opens the possibility of producing LOX for propellant. Water is also a useful radiation shielding material , and valuable to replenish expendables (water and oxygen) required for habitation in space. Because of the strong function of water vapor pressure with temperature, heating soil effectively liberates water vapor by sublimation. Microwave energy will penetrate soil and heat from within much more efficiently than heating from the surface with radiant heat. This is especially true under vacuum conditions since the heat transfer rate is very low. The depth of microwave penetration is a strong function of the microwave frequency and to a lesser extent on soil dielectric properties. Methods for complex electric permittivity and magnetic permeability measurement are being developed and used for measurements of lunar soil simulants. A new method for delivery of microwaves deep into a planetary surface is being prototyped with laboratory experiments and modeled with COMSOL MultiPhysics. We are planning to set up a planetary testbed in a large vacuum chamber in the coming year. Recent results are discussed.


45th AIAA Aerospace Sciences Meeting and Exhibit | 2007

Fluid Merging Viscosity Measurement (FMVM) Experiment on the International Space Station

Basil N. Antar; Edwin C. Ethridge; Daniel Lehman; William F. Kaukler

The concept of using low gravity experimental data together with fluid dynamical numerical simulations for measuring the viscosity of highly viscous liquids was recently validated on the International Space Station (ISS). After testing the proof of concept for this method with parabolic flight experiments, an ISS experiment was proposed and later conducted onboard the ISS in July, 2004 and subsequently in May of 2005. In that experiment a series of two liquid drops were brought manually together until they touched and then were allowed to merge under the action of capillary forces alone. The merging process was recorded visually in order to measure the contact radius speed as the merging proceeded. Several liquids were tested and for each liquid several drop diameters were used. It has been shown that when the coefficient of surface tension for the liquid is known, the contact radius speed can then determine the coefficient of viscosity for that liquid. The viscosity is determined by fitting the experimental speed to theoretically calculated contact radius speed for the same experimental parameters. Experimental and numerical results will be presented in which the viscosity of different highly viscous liquids were determined, to a high degree of accuracy, using this technique.


Review of Scientific Instruments | 1984

Technique for the efficient and reproducible fabrication of electromagnetic levitation coils

Edwin C. Ethridge; Peter A. Curreri; J. Theiss; G. J. Abbaschian

A technique has been developed for fabricating electromagnetic induction coils in a reproducible manner. The process utilizes a split mandrel that can be disassembled to remove the mandrel from the coil. The technique has increased coil production rates by a factor of 8 over the freehand winding method. The success rate for producing a functional levitation coil has been increased from 50% to 95%. The levitation coil designed during this work has successfully levitated and melted a variety of alloys including Cu, Ag, Ag–Ni, Cu–Fe, Fe–C, and Nb–Ge. W was also levitated but not melted at temperatures as high as 2700 °C. The highest sample melt temperature achieved was 2400 °C for the Nb–Ge samples.


50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition | 2012

Finite Element Analysis of Three Methods for Microwave Heating of Planetary Surfaces

Edwin C. Ethridge; William F. Kaukler

In-Situ Resource Utilization will be Ground Breaking technology for sustained exploration of space. Volatiles are present in planetary regolith, but water by far has the most potential for effective utilization. The presence of water at the lunar poles and Mars opens the possibility of using the hydrogen for propellant on missions beyond Earth orbit. Likewise, the oxygen could be used for in-space propulsion for lunar ascent/descent and for space tugs from low lunar orbit to low Earth orbit. Water is also an effective radiation shielding material as well as a valuable expendable (water and oxygen) required for habitation in space. Because of the strong function of water vapor pressure with temperature, heating regolith effectively liberates water vapor by sublimation. Microwave energy will penetrate soil and heat from within, much more efficiently than heating from the surface with radiant heat. This is especially true under vacuum conditions since the heat transfer rate is very low. The depth of microwave penetration is a strong function of the microwave frequency and to a lesser extent on regolith dielectric properties. New methods for delivery of microwaves into lunar and planetary surfaces is being prototyped with laboratory experiments and modeled with COMSOL MultiPhysics. Recent results are discussed.


MRS Proceedings | 1981

Properties of a Constricted-Tube Air-Flow Levitator

J. E. Rush; W. K. Stephens; Edwin C. Ethridge

The properties of a constricted-tube gas flow levitator first developed by Berge et al. (1981) have been investigated experimentally in order to predict its behavior in a gravity-free environment and at elevated temperatures. The levitator consists of a constricted (quartz) tube fed at one end by a source of heated air or gas. A spherical sample is positioned by the air stream on the downstream side of the constriction, where it can be melted and resolidified without touching the tube. It is shown experimentally that the kinematic viscosity is the important fluid parameter for operation in thermal equilibrium at high temperatures. If air is heated from room temperature to 1200 C, the kinematic viscosity increases by a factor of 14. To maintain a given value of the Reynolds number, the flow rate would have to be increased by the same factor for a specific geometry of tube and sample. Thus, to maintain stable equilibrium, the flow rate should be increased as the air or other gas is heated. The other stability problem discussed is associated with changes in the shape of a cylindrical sample as it melts.


47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition | 2009

Extraction of Water from Polar Lunar Permafrost with Microwaves - Dielectric Property Measurements

Edwin C. Ethridge; William F. Kaukler

Remote sensing indicates the presence of hydrogen rich regions associated with the lunar poles. The logical hypothesis is that there is cryogenically trapped water ice located in craters at the lunar poles. Some of the craters have been in permanent darkness for a billion years. The presence of water at the poles as well as other scientific advantages of a polar base, have influenced NASA plans for the lunar outpost. The lunar outpost has water and oxygen requirements on the order of 1 ton per year scaling up to as much as 10 tons per year. Microwave heating of the frozen permafrost has unique advantages for water extraction. Proof of principle experiments have successfully demonstrated that microwaves will couple to the cryogenic soil in a vacuum and the sublimed water vapor can be successfully captured on a cold trap. The dielectric properties of lunar soil will determine the hardware requirements for extraction processes. Microwave frequency dielectric property measurements of lunar soil simulant have been measured.

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William F. Kaukler

University of Alabama in Huntsville

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Dennis S. Tucker

Marshall Space Flight Center

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Peter A. Curreri

Marshall Space Flight Center

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Basil N. Antar

University of Tennessee Space Institute

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Houssam Toutanji

University of Alabama in Huntsville

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Guy A. Smith

University of Alabama in Huntsville

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C. A. McLemore

Marshall Space Flight Center

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Christopher M. Goff

University of Alabama in Huntsville

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D. Maxwell

University of Tennessee Space Institute

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