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DEVELOPMENT OF FERRITIC STAINLESS STEEL-UO$sub 2$ DISPERSION FUEL ELEMENTS (open access)

DEVELOPMENT OF FERRITIC STAINLESS STEEL-UO$sub 2$ DISPERSION FUEL ELEMENTS

A preliminary definition of a fabrication process for ferritic stainless steel-UO/sub 2/ fuel clad with Type 430 stainiess steel has been achieved. The procedure is an adaptation of an earlier process for preparing austenitic fuel elements, and consists of the cold-binder extrusion of a plastic powder dispersion which is fired in dry hydrogen, fitted with welded end caps, and electroplated with nickel. This core is inserted into a length of type 430 stainless steel cladding and the assembly is bonded by hot-swaging at 800 C. The irradiation performance of such a fuel element was examined by means of an MTR test. The results of this test strongly indicated that the desired lowering of UO/sub 2/ particle operating temperature was realized and that ferritic stainless steel is not unduly susceptible to irradiation dannage. (auth)
Date: January 30, 1958
Creator: Barney, W.K.; Ray, W.E. & Sowman, H.G.
System: The UNT Digital Library
Experimental and Theoretical Determination of Forces and Moments on a Store and on a Store- Pylon Combination Mounted on a 45 Degree Swept- Wing-Fuselage Configuration at a Mach Number of 1.61 (open access)

Experimental and Theoretical Determination of Forces and Moments on a Store and on a Store- Pylon Combination Mounted on a 45 Degree Swept- Wing-Fuselage Configuration at a Mach Number of 1.61

Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in supersonic pressure tunnel. The results of the investigation indicate that the most important source of store-pylon side forces is the pylon itself.
Date: January 30, 1958
Creator: Morris, Odell A.; Carlson, Harry W. & Geier, Douglas J.
System: The UNT Digital Library
Performance of an Inlet Having a Variable-angle Two-dimensional Compression Surface and a Fixed-geometry Subsonic Diffuser for Application to Reduced Engine Rotative Speeds- Mach Numbers 0.66, 1.5, 1.7, and 2.0 (open access)

Performance of an Inlet Having a Variable-angle Two-dimensional Compression Surface and a Fixed-geometry Subsonic Diffuser for Application to Reduced Engine Rotative Speeds- Mach Numbers 0.66, 1.5, 1.7, and 2.0

Report presenting the performance of a two-dimensional side inlet with a technique of varying compression-surface angle while retaining a fixed-geometry diffuser at several Mach numbers and zero angle of attack. A 12 degree compression ramp was faired into the diffuser contour in this conventional manner. Results regarding the inlet flow field, application to reduced engine speeds, and a inlet performance with a sudden expansion in the diffuser are provided.
Date: January 30, 1958
Creator: Allen, John L.
System: The UNT Digital Library
PRELIMINARY ZIRCONIUM ALLOY DATA FROM LOOP L-2-17 (open access)

PRELIMINARY ZIRCONIUM ALLOY DATA FROM LOOP L-2-17

Core specimens of Zr alloys such as Nb--Zr and Fe-Nb-Zr were in-pile corrosion tested. Operating conditions are summarized for these and former similar tests. The corrosion solution contained UO/sub 2/SO/sub 4/, CuSO/sub 4/, and H/sub 2/SO/sub 4/, with a make-up solution composed of UO/sub 2/SO/sub 4/, CuSO/sub 4/, H/sub 2/SO/sub 4/, and Cr. Corrosion rites ire tabulated and presented graphically. (J.R.D.)
Date: January 30, 1958
Creator: Baker, J.E.
System: The UNT Digital Library
PERFORMANCE OF THE TBP PROCESS FOR ALUMINUM FUELS IDAHO CHEMICAL PROCESSING PLANT, 1955-1956 (open access)

PERFORMANCE OF THE TBP PROCESS FOR ALUMINUM FUELS IDAHO CHEMICAL PROCESSING PLANT, 1955-1956

Observations of the performance of the Idaho Chemical Processing Plant as modified for continuous dissolution and TBP lst cycle extraction, as to process chemistry and process engineering are reported for the initial plantscale full-irradiation-level operating run. As-operated flowsheets, the results of plant scale tests of the continuous dissolver, and fission prcduct decontamination data are emphasized. (auth)
Date: January 30, 1958
Creator: Rohde, K. L.
System: The UNT Digital Library
Longitudinal Stability Investigation of a Vertical-Take-Off-and-Landing Airplane Configuration With Simulated Jet Intake and Exhaust at Mach Numbers of 1.61 and 2.01 (open access)

Longitudinal Stability Investigation of a Vertical-Take-Off-and-Landing Airplane Configuration With Simulated Jet Intake and Exhaust at Mach Numbers of 1.61 and 2.01

Report presenting an investigation of a semispan model of a possible vertical-take-off-and-landing jet bomber configuration at a range of Mach numbers. The primary objective was to determine to the effects of jet interference, horizontal-tail location, and canard controls on the longitudinal stability characteristics of the model.
Date: January 30, 1958
Creator: Lord, Douglas R.
System: The UNT Digital Library
Exit Beam Trajectories for the Cambridge Electron Accelerator (open access)

Exit Beam Trajectories for the Cambridge Electron Accelerator

"A method is outlined for calculating the trajectories, through the magnetic field of the following magnet pair of positive and negative particles of different momenta produced in a target. Representative trajectories were computed by this method and are given numerically."
Date: January 30, 1958
Creator: Steffen, K. G.
System: The UNT Digital Library