Resource Type

ELEMENT 98 (open access)

ELEMENT 98

Definite identification has been made of an isotope of the element with atomic number 98 through the irradiation of Cm{sup 242} with 35 Mev helium ions in the Berkeley Orocker Laboratory 60-inch cyclotron. The isotope which has been identified has an observed half-life of about 45 minutes and probably has the mass number 244. The observed mode of decay of the 98{sup 244} is through the emission of alpha-particles, with energy about 7.1 Mev, which agrees with predictions, and other considerations involving the systematics of radioactivity in this region indicate that it should also be unstable toward decay by electron-capture. The chemical separation and identification of the new element was accomplished through the use of ion exchange adsorption methods employing the resin Dowex-50. The element 98 isotope appears in the eka-dysprosium position on elution curves containing 4.6-hour Bk{sup 243} (formed by a d,n reaction in the same bombardment) and the bombarded Cm{sup 242} as reference points; that is, it preceded berkelium and curium off the column just as dysprosium precedes terbium and gadolinium. The experiments so far have revealed only the tripositive oxidation state of eka-dysprosium character but practically no attempts at oxidation to possible IV and V states have …
Date: February 27, 1950
Creator: Thompson, S. G.; Street Jr., K.; Ghiorso, A. & Seaborg, G. T.
System: The UNT Digital Library
Refractories for Continuous Reduction of Uranium (open access)

Refractories for Continuous Reduction of Uranium

Report presenting a study that evaluates various types of refractories for use in a refractory-lined vessel that would be used for continuous reduction of uranium tetrafluoride to uranium metal.
Date: February 27, 1956
Creator: Smalley, Allison K.; Hyde, Collin; Allison, Adrian G. & Duckworth, Winston Howard
System: The UNT Digital Library
Aircraft Nuclear Propulsion Project Quarterly Progress Report for Period Ending December 10, 1950 (open access)

Aircraft Nuclear Propulsion Project Quarterly Progress Report for Period Ending December 10, 1950

Technical report detailing expansion of the Aircraft Nuclear Propulsion at the Oak Ridge National Laboratory. Major facilities completed at this time were the Shielding Rector, the ANP Critical Facility, and the 86-in. Cyclotron. Outlines further need for radiation damage studies. [From Summary]
Date: February 27, 1951
Creator: Briant, R. C.; Ellis, C. B. & Cottrell, W. B.
System: The UNT Digital Library
A Method for the Analysis of Radionuclide Mixture Using a Gamma-Beta Scintillation Spectrometer (open access)

A Method for the Analysis of Radionuclide Mixture Using a Gamma-Beta Scintillation Spectrometer

The following report describes a beta and gamma scintillation detector similar to what was used in previous decay studies, yet was modified to make it suitable for the analysis of mixtures of radio-nuclides.
Date: February 27, 1953
Creator: Leboeuf, M. B. & Connally, R. E.
System: The UNT Digital Library
Activity of fission products as a function of decay time, and relationship to the TBP process (open access)

Activity of fission products as a function of decay time, and relationship to the TBP process

Fission product distribution, fission product activities, and decontamination factors are terms of general usage in the Chemical Development Section. Specific values for some of these terms have been based upon data procured several years ago. In many cases more accurate basic numbers are now available. This report sets forth in tabular form detailed information on fission product activities as a function of decay time for certain conditions. It attempts to quality the use of the theoretical curie as a unit of activity to a unit having a more direct practical significance, the ``countable curie.``
Date: February 27, 1950
Creator: Schwennesen, J. L.
System: The UNT Digital Library
Beneficiation of Monument Number 2 Ore Apache County, Arizona (open access)

Beneficiation of Monument Number 2 Ore Apache County, Arizona

From introduction: The Monument No. 2 mine is in the Navajo Indian Reservation, Apache County, Arizona, about 20 miles southwest from the San Juan River at Mexican Hat, Utah, and 26 miles southwest from Mexican Water, Arizona. The property has been operated, since its discovery, by Vanadium Corporation of America, which holds a 10-year mining lease, granted through the Interior Department, to 43 acres of ground. History of the discovery of the deposit is vague, but reportedly it was first seen around 1942 by a Navajo who mentioned the occurrence to Harry Goulding, Indian trader, who in turn advised D. W. Viles of Vanadium Corporation of America. Minor portions of the deposit are held by Cato Sells and Harvey Black, Navajos, under mining permits issued by the Navajo Tribal Council. The Sells acreage is being operated by Climax Uranium Corporation.
Date: February 27, 1952
Creator: Sheridan, M. J.
System: The UNT Digital Library
Antiproton Interaction Cross Sections (open access)

Antiproton Interaction Cross Sections

Using the 1.19-Bev/c antiproton beam recently discovered at the Berkeley Bevatron of the University of California, we have measured the attenuation cross section in beryllium and copper. These cross sections are compared to attenuation measurements made with the same geometry using positive protons of the same incident energy (497 MeV).
Date: February 27, 1956
Creator: Chamberlain, Owen; Keller, Donald V.; Segre, Emilio; Steiner,Herbert M.; Wiegand, Clyde & Ypsilantis, Tom
System: The UNT Digital Library
Observations on the Radiation Decomposition of Some C14 LabeledCompounds (open access)

Observations on the Radiation Decomposition of Some C14 LabeledCompounds

Varying amounts of radiation decomposition during storage in the dry form have been found in the cases of C{sup 14}-labeled valine, norvaline, norleucine, choline chloride, calcium glycolate and cholesterol. These data indicate that investigators using labeled organic compounds should make frequent checks of the purity of these compounds in order to exclude the possibility of the presence of decomposition products.
Date: February 27, 1953
Creator: Tolbert, B.M.; Adams, P.T.; Bennett, Edward L.; Hughes, Ann M.; Kirk, Martha R.; Lemmon, R.M. et al.
System: The UNT Digital Library
SEMI-ANNUAL SUMMARY RESEARCH REPORT IN ENGINEERING FOR JULY-DECEMBER 1955 (open access)

SEMI-ANNUAL SUMMARY RESEARCH REPORT IN ENGINEERING FOR JULY-DECEMBER 1955

None
Date: February 27, 1956
Creator: unknown
System: The UNT Digital Library
BOUNDARY CONDITIONS AND CONSERVATION PROPERTIES OF FOPP, A PLASMA FOKKER- PLANCK CODE (open access)

BOUNDARY CONDITIONS AND CONSERVATION PROPERTIES OF FOPP, A PLASMA FOKKER- PLANCK CODE

The energy distribution of ions and electrons in DCX are being studied by means of the Fokker-Planck approximation to the Boltzmann equation. An IBM- 704 code, called FOPP, was constructed to solve simultaneously the coupled Fokker-Planck equations for each of the two species of particles. This report discusses the difference scheme employed and derives the boundary conditions necessary in order that this difference scheme conserve energy and particles in the absence of sources and sinks. In particular, detailed discussion is given of problems arising from the use of two grid sizes, which proved advantageous on account of the great difference in the mass of ions and electrons. (auth)
Date: February 27, 1959
Creator: Fowler, T.K.; Rankin, F.M. & Simon, A.
System: The UNT Digital Library
SEMI-PILOT OPERATION OF THE AMMONIUM CARBONATE LEACHING PROCESS (open access)

SEMI-PILOT OPERATION OF THE AMMONIUM CARBONATE LEACHING PROCESS

None
Date: February 27, 1956
Creator: Hollis, E.T.
System: The UNT Digital Library
Some Factors Influencing the Use of Tributyl Phosphate for the Extraction of Uranium in Analysis (open access)

Some Factors Influencing the Use of Tributyl Phosphate for the Extraction of Uranium in Analysis

None
Date: February 27, 1951
Creator: Bartlett, T. W.
System: The UNT Digital Library
Aerodynamic principles for the design of jet-engine induction systems (open access)

Aerodynamic principles for the design of jet-engine induction systems

From Introduction: "It is the purpose of this report to assemble principles of induction-system design for flight to a Mach number of 2 and to use existing data to show the consequences of compromising them."
Date: February 27, 1956
Creator: Davis, Wallace F. & Scherrer, Richard
System: The UNT Digital Library
Tabulated pressure data for several flap-type trailing edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01 (open access)

Tabulated pressure data for several flap-type trailing edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01

Report presenting an investigation at two Mach numbers for a range of Reynolds numbers to determine the pressure distributions at several spanwise stations for a series of 25.4-percent-chord trailing-edge controls on a trapezoidal wing with a 23 degree sweptback leading edge, aspect ratio of 3.1, and taper ratio of 0.4. The report contains the tabulated pressure data for the complete range of test variables.
Date: February 27, 1956
Creator: Lord, Douglas R. & Czarnecki, K. R.
System: The UNT Digital Library
Aerodynamic Principles for the Design of Jet-Engine Induction Systems (open access)

Aerodynamic Principles for the Design of Jet-Engine Induction Systems

Jet engine induction systems investigations and relationship of air inlets, drag, airframe, pressure recovery, flow and interferences.
Date: February 27, 1956
Creator: Davis, Wallace F. & Scherrer, Richard
System: The UNT Digital Library
Turbojet-engine evaluation of AISI 321 and AISI 347 stainless steels as nozzle-blade materials (open access)

Turbojet-engine evaluation of AISI 321 and AISI 347 stainless steels as nozzle-blade materials

Report presenting an investigation to evaluate the engine service performance of nozzle-diaphragm blades of AISI 321 and AISI 347 stainless steels. Data were obtained from three nozzle diaphragms alternately bladed with each of the two materials. Results regarding a visual inspection, a metallurgical examination, the mechanism of cracking, and the classification of failures are provided.
Date: February 27, 1950
Creator: Garrett, Floyd B. & Yaker, Charles
System: The UNT Digital Library
Transonic Characteristics of a 45 Degree Sweptback Wing-Fuselage Combination: Effect of Longitudinal Wing Position and Division of Wing and Fuselage Forces and Moments (open access)

Transonic Characteristics of a 45 Degree Sweptback Wing-Fuselage Combination: Effect of Longitudinal Wing Position and Division of Wing and Fuselage Forces and Moments

Report presenting an investigation on a body of revolution with a sweptback wing with a 0.25-mean-aerodynamic-chord point at the maximum body diameter and 1.2 mean aerodynamic chords behind the maximum diameter. The fuselage had a fineness ratio of 10, a 45 degree swept wing with an aspect ratio of 4.0, a taper ratio of 0.6, and NACA 65A006 airfoil sections parallel to the plane of symmetry. Lift, drag, pitching moments, and angles of attack were measured at a range of Mach numbers.
Date: February 27, 1953
Creator: Hallissy, Joseph M. & Bowman, Donald R.
System: The UNT Digital Library
Pressure Recovery, Drag, and Subcritical Stability Characteristics of Three Conical Supersonic Diffusers at Stream Mach Numbers From 1.7 to 2.0 (open access)

Pressure Recovery, Drag, and Subcritical Stability Characteristics of Three Conical Supersonic Diffusers at Stream Mach Numbers From 1.7 to 2.0

A study of a 20 degree and a 25 degree half-angle high mass-flow ratio conical supersonic inlet was made on a 16-inch ram jet in the 8- by 6-foot supersonic tunnel. A greater range of stable subcritical operation was obtained with the low mass-flow ratio inlets; a greater range was obtained with the 25 degree than with the 20 degree half-angle low mass-flow ratio inlet. The high mass-flow ratio inlet had the least drag.
Date: February 27, 1952
Creator: Nussdorfer, Theodore J.; Obery, Leonard J. & Englert, Gerald W.
System: The UNT Digital Library
Preliminary Investigation of the Combustion of Pentaborane and Diborane in a Turbojet Combustor at Simulated Altitude Conditions (open access)

Preliminary Investigation of the Combustion of Pentaborane and Diborane in a Turbojet Combustor at Simulated Altitude Conditions

Report presenting an investigation to determine the combustion characteristics of pentaborane and diborane in a turbojet combustor. Four different test conditions were explored, which varied in inlet total pressure, temperature, and simulated flight conditions. Results regarding the combustor itself and performance of diborane fuel at high altitude are provided.
Date: February 27, 1957
Creator: Gibbs, J. B.; Kaufman, W. B. & Branstetter, J. R.
System: The UNT Digital Library
MEDICAL AND HEALTH PHYSICS QUARTERLY REPORT OCTOBER, NOVEMBER, AND DECEMBER 1950 (open access)

MEDICAL AND HEALTH PHYSICS QUARTERLY REPORT OCTOBER, NOVEMBER, AND DECEMBER 1950

None
Date: February 27, 1951
Creator: unknown
System: The UNT Digital Library
Boilout experiment (open access)

Boilout experiment

There is a definite need to determine the time required for the water in a process tube to boil out after loss of inlet flow. This information is required to evaluate the reactivity and power transients following such an occurrence. Such information will also partially determine the incentive for improvements in safety circuits and equipment, accelerated safety rods in particular. A secondary objective is to learn more about the mechanism of the boil-out. Boil-out times have been theoretically predicted in the past with very little experimental data to back them up. A scanning capacitance method is presented for measurement of the water distribution within a process tube under transient boiling conditions. Preliminary results of exploratory runs are included. The runs simulate inlet pigtail failures on process tubes operating at 725 and 1,000 KW. Curves of water distribution over the tube with time and total tube water content are included. Recommendations are made that the tests be continued to provide valid data for assessing the reactor hazards involved in cases of cooling water supply failure.
Date: February 27, 1957
Creator: Pound, D. C.
System: The UNT Digital Library
SM-2 VAULT CRITICALITY (open access)

SM-2 VAULT CRITICALITY

To determine the safety of the array in the storage vault for the SM-2 experimental fuel plates, two criticality criteria were applied. A maximum of 18 fuel plates was stored in sthainless steel tubes and the tubes belted to a frame on the wall to prevent movement. No tube could go critical by itseIf. The vauit was then assumed completely flooded by water. In the first calculation, the fuel array was assumed to be distributed uniformly over the wall forming a large slab. This method indicated the array might be critical if the steel tube and cadmium lining were neglected. In the second method, a conservative calculation, wnich included the steel tube and cadmium lining was made. This method indicataed the array was subcritical. Calculations were then made of the criticalty of the SM-2 vault without the steel--cadmium tubes and wcoden blocks. The multiplication factor of the vault was also calculated. In order to determine the accuracy of these calculations, an ORNL critical experimental array was calculated applying the same analytical techniques. (M.C.G.)
Date: February 27, 1959
Creator: Fried, B.E.
System: The UNT Digital Library
Fuel Cycle Costs in a Graphite Moderated U$sup 235$-Th Fueled Fused Salt Reactor (open access)

Fuel Cycle Costs in a Graphite Moderated U$sup 235$-Th Fueled Fused Salt Reactor

A fuel-cycle economic study was made for a 315-Mw(e) graphite-moderated U/sup 235/-Th-fueled fused-salt reactor. Fuel cycle costs of approximately 1.3 mills/kwh may be possible for such reactors when reprocessed for U/sup 233/ and U/ sup 235/ recover y at the end of a 9-year cycle. Continuous removal of fission products during the reactor cycle does not appear to offer any great economic advantage for the converter reactor considered. (auth)
Date: February 27, 1959
Creator: Guthrie, C. E.
System: The UNT Digital Library