Resource Type

States

Second Report on Liquid Metal Level Instrument (open access)

Second Report on Liquid Metal Level Instrument

The liquid metal level instrument will operate at tank temperatures up to 1000 F. Overall system accuracy depends on operating conditions, as described in the report. Test accuracies from 2 to 8% have been obtained from full to empty tank. The primary detector unit successfully passed navy HI shock test.
Date: December 21, 1954
Creator: Droma, Clarence R.
Object Type: Report
System: The UNT Digital Library
LMFR Progress Letter for April 1954 (open access)

LMFR Progress Letter for April 1954

Summary of miscellaneous updates related to the project. This includes information on the following. Simplified equations for modeling reactor conditions. Solubility tests involving thorium, bismuth, and protactinium. various other measurements and tests involving thorium, uranium, protactinium, bismuth, aluminum, and various other salts.
Date: May 21, 1954
Creator: Miles, F. T.
Object Type: Report
System: The UNT Digital Library
Hanford Atomic Products Operation monthly report, April 1954 (open access)

Hanford Atomic Products Operation monthly report, April 1954

This is a progress report of the production reactors on the Hanford Reservation for the month of April 1954. This report takes each division (e.g., manufacturing, medical, accounting, occupational safety, security, reactor operations, etc.) of the site and summarizes its accomplishments and employee relations for that month.
Date: May 21, 1954
Creator: McCune, F. K.
Object Type: Report
System: The UNT Digital Library
The corrosion of Hanford fuel elements: Method for the treatment and analyses of in-pile corrosion data (open access)

The corrosion of Hanford fuel elements: Method for the treatment and analyses of in-pile corrosion data

The corrosion rates of slug jackets exposed in the Hanford piles are monitored to determine optimum operating conditions and to evaluate proposed changes in process specifications. Selected process tubes are charged with weighed slugs, and the coolant flow rate and temperature rise through the tubes are recorded until the slugs are discharged. The corrosion rates of these control slugs are computed from weight loss data after discharge. The data obtained in this manner are used to find the relationship between slug jacket corrosion rates and the various conditions of power and temperature that are encountered in the piles. This report covers all of the corrosion data obtained to date for slugs that have been cooled with the currently specified process water, which is alum-coagulated and contains 2 ppm sodium dichromate as an inhibitor (see Appendix II for the water composition). All of the slugs were normal production pieces canned in 2-S aluminum.
Date: December 21, 1954
Creator: DeHalas, D. R.
Object Type: Report
System: The UNT Digital Library
Table Top 1 Circuitry (open access)

Table Top 1 Circuitry

Abstract: "This is a detailed report on the circuitry, the electrical components, and the electrical engineering problems of Table Top I, the 140-kilojoule experimental model of a magnetic mirror machine being developed at the University of California Radiation Laboratory, Livermore."
Date: July 21, 1954
Creator: Cummings, David B. & Wharton, Charles B.
Object Type: Report
System: The UNT Digital Library
Response of Pressure Gauges to Dust-Laden Shock Waves (open access)

Response of Pressure Gauges to Dust-Laden Shock Waves

"A series of shock tube studies demonstrate that two types of pressure gauges respond to dust carried with shock waves by indicating an increase in dynamic pressure. This contribution to the dynamic pressure is approximately the product of the dust density and the square of the dust velocity under the experimental conditions. Besides this information studies give insight into the interaction of a square shock wave with dust when that dust is placed in a plane before and parallel to the shock front. It is found that the shape of the pressure wave is little changed except for a rounding of the front. The dust, after accelerating, is carried as a pulse with the mass flow velocity of the air."
Date: 1954-05-21?
Creator: Banister, John Robert & Broyles, C. D.
Object Type: Report
System: The UNT Digital Library
The Tensile Strength of Solid-State Bonded Aluminum and Nickel-Plated Uranium (open access)

The Tensile Strength of Solid-State Bonded Aluminum and Nickel-Plated Uranium

To aid in the evaluation of solid-state bending techniques for cladding natural-uranium fuel-element cores with aluminum, tensile specimens, 1/4 in. in diameter and 3 in. long were made and tested. Results show that these techniques are capable of producing satisfactory bonds between aluminum and nickel-plated uranium. Pressing conditions of 1 min at 950F and 6000 psi produced consintent bond strengths equal to the yield strength of 25 aluminum. When optimum bonding conditions are used, anodic activation and strike-current density are not critical to bond strength. Nickel plating of the aluminum component of the bond couple reduced the tensile strength by about 50%. (auth)
Date: October 21, 1954
Creator: Saller, H. A.; Dickerson, R. F. & Carlson, R. J.
Object Type: Report
System: The UNT Digital Library
Transformation Kinetics of Uranium-Molybdenum Alloys (open access)

Transformation Kinetics of Uranium-Molybdenum Alloys

None
Date: October 21, 1954
Creator: Saller, H. A.; Rough, F. A. & Bauer, A. A.
Object Type: Report
System: The UNT Digital Library
Quarterly Summary Research Report in Physics for July, August, and September 1954 (open access)

Quarterly Summary Research Report in Physics for July, August, and September 1954

None
Date: December 21, 1954
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Development of the Amex process for americium recovery (open access)

Development of the Amex process for americium recovery

None
Date: May 21, 1954
Creator: Rainey, R.H.
Object Type: Report
System: The UNT Digital Library
A Proposed Fuel Element (open access)

A Proposed Fuel Element

None
Date: July 21, 1954
Creator: Daane, Robert
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: MS-154 (open access)

Texas Attorney General Opinion: MS-154

Letter opinion issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification; Authority of a Commissioners' Court to levy §.30 ad valorem tax for farm to market roads or flood control under the provisions of Section 1-a of Article 8 of the Texas Constitution when the State Automatic Tax Board is making the State levy in portions of the county during the duration of a tax donation.
Date: September 21, 1954
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-166 (open access)

Texas Attorney General Opinion: MS-166

Letter opinion issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification;Retention of mineral rights in sale of land acquired by an independent school district in a delinquent tax suit.
Date: December 21, 1954
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Longitudinal Stability and Control of the Model Equipped with a Supersonic-Type Elliptical Wing-Root Inlet (open access)

Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Longitudinal Stability and Control of the Model Equipped with a Supersonic-Type Elliptical Wing-Root Inlet

Memorandum presenting development tests on a 1/4-scale model of the Republic F-105 airplane in the 19-foot pressure tunnel. The tests in this particular report include longitudinal stability and control tests of the basic design provided by the contractor, tests of various modifications designed to improve the stability characteristics of the model with the trailing-edge flaps deflected, brief exploratory lateral-control and rudder-effectiveness tests, and stall studies and duct air-flow measurements.
Date: July 21, 1954
Creator: Kelly, H. Neale & Cancro, Patrick A.
Object Type: Report
System: The UNT Digital Library
Rocket-model investigation of the longitudinal stability and drag characteristics of a 1/10-scale model of the Convair XF2Y-1 airplane having open ducts and the elevons deflected upward 3.5 degrees: TED No. NACA DE 375 (open access)

Rocket-model investigation of the longitudinal stability and drag characteristics of a 1/10-scale model of the Convair XF2Y-1 airplane having open ducts and the elevons deflected upward 3.5 degrees: TED No. NACA DE 375

Report presenting flight testing of a scale rocket-propelled model of the Convair XF2Y-1 airplane with open ducts and elevons deflected upward 3.5 degrees through a range of Mach numbers. Report presenting lift and stability, drag, and duct flow are provided.
Date: January 21, 1954
Creator: Welsh, Clement J.; Bland, William M., Jr. & Walters, Richard E.
Object Type: Report
System: The UNT Digital Library
A Wind-Tunnel Investigation of the Use of Spoilers for Obtaining Static Longitudinal Stability of a Canard-Missile Model in Reverse Flight (open access)

A Wind-Tunnel Investigation of the Use of Spoilers for Obtaining Static Longitudinal Stability of a Canard-Missile Model in Reverse Flight

Report presenting an investigation in the stability tunnel of the use of spoilers for obtaining static longitudinal stability of a model of a canard missile in reverse flight. Results indicated that stable pitching-moment slopes can be obtained at angles of attack up to 11 degrees in the low speed range of the tests, but further investigation of high subsonic speeds will be necessary.
Date: June 21, 1954
Creator: Fletcher, Herman S.
Object Type: Report
System: The UNT Digital Library
An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash Behind Five Pointed-Tip Wings at Supersonic Speeds (open access)

An Analysis of Pressure Studies and Experimental and Theoretical Downwash and Sidewash Behind Five Pointed-Tip Wings at Supersonic Speeds

The following report covers an investigation that was done to supplement available experimental data on flow fields behind wings of an aircraft at supersonic speeds, as well as to furnish more quantitative information on the choice of the theoretical method for a given configuration and the accuracy to be expected when using such a method.
Date: April 21, 1954
Creator: Boatright, William B.
Object Type: Report
System: The UNT Digital Library
Effect of Nozzle Contour on Drag of Parabolic Afterbodies (open access)

Effect of Nozzle Contour on Drag of Parabolic Afterbodies

Memorandum presenting an investigation of the effect of nozzle internal contour on afterbody drag in the 8- by 6-foot supersonic wind tunnel. Five different nozzle-afterbody configurations were evaluated. Results regarding the boattail pressure drag, base drag, and total drag are provided.
Date: June 21, 1954
Creator: Vargo, Donald J. & Englert, Gerald W.
Object Type: Report
System: The UNT Digital Library
Effect of immersed surfaces in combustion zone on efficiency and stability of 5-inch diameter ram-jet combustor (open access)

Effect of immersed surfaces in combustion zone on efficiency and stability of 5-inch diameter ram-jet combustor

Report presenting an extension of previous work on immersed surfaces in the combustion zone of a ramjet engine. The primary focus was to determine the effect of combustion efficiency and stability of blades located within the immediate wake of a V-gutter flame holder and to find some location and orientation of blades for optimum combustion efficiency and improved stability limits with a minimum of pressure loss.
Date: June 21, 1954
Creator: Reynolds, Thaine W. & Male, Donald W.
Object Type: Report
System: The UNT Digital Library
Analysis of Factors Affecting Selection and Design of Air-Cooled Single-Stage Turbines for Turbojet Engines 2: Analytical Techniques (open access)

Analysis of Factors Affecting Selection and Design of Air-Cooled Single-Stage Turbines for Turbojet Engines 2: Analytical Techniques

Memorandum presenting computation methods for analyzing turbojet-engine performance for a series of air-cooled nonafterburning and afterburning engines where all the engine components are simultaneously aerodynamically limited. The coolant-flow ratio was arbitrarily assigned so that the results of the analysis can be applied to any specific air-cooled blade configurations.
Date: June 21, 1954
Creator: Rossbach, Richard J.
Object Type: Report
System: The UNT Digital Library
A method of measuring jet thrust of turbojet engines in flight installations (open access)

A method of measuring jet thrust of turbojet engines in flight installations

"Measurement of the jet thrust of a turbojet engine in flight becomes more difficult as the number and complexity of the engine components increase. It is desirable, therefore, that a general correlation of jet thrust be developed which is applicable to a simple direct reading thrustmeter. In view of this need a correlation is presented which is independent of flight conditions and applicable to both non-afterburning and afterburning engines equipped with nonejector type fixed- and variable-area convergent exhaust nozzles" (p. 1)
Date: January 21, 1954
Creator: Sivo, Joseph N. & Fenn, David B.
Object Type: Report
System: The UNT Digital Library