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ANP QUARTERLY PROGRESS REPORT STAINLESS STEEL MELT TUBE FABRICATED FROM SCH 40 I-in -IPS PIPE conductivity relation developed for the fluoride mixtures previously studied. The solid and liquid thermal conductivity measurements of NaF-KF-LiF (11.5-42-46.5 mole %) and NaF-KF-LiF-UF, (10.9-43.5-44.5-1.1 mole %) were reported in part in previous quarterlies. All conductivity data obtained with several types of onductivity devices for these two fluoride mixtures are shown in Fig. 8.5. The liquid and solid conductivity values of the ternary fluoride mixture are nearly the same, and the same is true of the quaternary. 118 ~ CHROMEL-ALUMEL THERMOCOUPLES (4) Fig. 8.3. Furnace for Viscosity Measurements. O V UNCLASSIFIED ORNL-LR-DWG 4454 OEin POSITION OF THERMOCOUPLE WELLS IN MELT TUBE WALL (CHROMEL-ALUMEL COUPLES IN 0.08-in.- OD STAINLESS STEEL WELLS) 110 v A longitudinal thermal conductivity apparatus has been designed and constructed for the meas- urement of the conductivity of metallic beryllium. It is essentially the same apparatus as that reported previously7 and is contained in an inert- gas-fi lled box to protect personnel from beryllium poi son i ng. 7W. D. Powers, S. J. Claiborne, and R. M. Burnett, ANP Quar. Prog. Rep. June 10, 1953, ORNL-1556, p 86. . - 2 .-
MADE AUG. 4953 TEMPERATURE (OK) SESRW. ORNL-LR-DWG 4455 300 400 500 700 too0 TEMPERATURE ("G) Fig. 8.4. Viscosity of NaF-ZrF,-UF, (53.5- 40-6.5 mole %). PERIOD ENDING DECEMBER 70,1954 -sum ORNL-LR-I)WG 4456 w NoF-KF-LiF NOF-KF-LIF-UF.~ - (11 5-42-46 5 mole %) (10.3-435-44 5-1.1 n~ole%I COOLING SPHERE (SOLIDI A A FLAT PLATE (SOLIDI l 0 VARIABLE GAP 0 " 0 (LIQUID1 500 I 1000 (500 TEMPERATURE (OF) Fig. 8.5. Thermal Conductivities of NaFc-KF-LiF and NaF=KF-LiF-UF, in the Liquid arid Solid States. 119
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ORNL DOCUMENT REFERENCE LIBRARY, Y-
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.. II 1. G. M. Adamson 2. R. G. Aff
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iv R ports pr ri ORNL-528 ORNL-629
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4 . CRITICAL EXPERIMENTS ..........
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Removal of Xe13' from Molten Fluori
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ANP QUARTERLY PROGRESS REPORT main
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ANP QUARTERLY PROGRESS REPORT 26OOC
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incident on crew shield sides and r
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1. CIRCULATING-FUEL AIRCRAFT REACTO
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clean reactor at a low power for a
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for more than 0.6 Mw in the sodium,
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I .o 08 0.6 . E - ‘z I - 0.4 0.2
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i PERIOD ENDING DECEMBER 70,7954 Fi
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Analytical studies, layout work, an
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XENON- REMOVAL SYSTEM 4 BLEED CIRCU
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c. . f 0 L .. would mean that most
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L . PERIOD ENDING DECEMBER 70, 7954
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PERIOD ENDING DECEMBER 70, 7954
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PERIOD ENDING DECEMBER 70, 7954 Fig
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A" d OIL IN-l OIL IN-2 NUCLEAR I N
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the floor up to 3 ft below the bolt
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" i' Design work is under way on an
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The pump has unusual ability to rem
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into operation with a Reynolds numb
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. . . . .- . Fig. 3.5. Heat Exchang
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TABLE 3.1. GAS-FIRED FURNACE OPERAT
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Fig. 4.1. Second Reflector-Moderate
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