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<br />10 C. This was accomplished by adjustment of each of the I-inch <br />calibration weights to exactly 823.6 g, equivalent to a water <br />density of 0.9999 g/cm3 which occurs at 0.5 and 7.50C. The <br />Belfort instruction manual (1976) states that each calibration <br />weight weighs 822.7 g and is equivalent to a volume of water one <br />inch deep by 8 inches in diameter (Belfort collector orifice <br />diameter). This would be correct at a temperature of either <br />-6.50 C. or +170 C, where the density of water is 0.9988 g/cm3. <br /> <br />The dual-traverse gages were calibrated on 6 October 1982 <br />over the full 12-inch range with cha:rt paper graduated in inches <br />(Chart No. 5-4047-B). <br /> <br />Individual cal ibration weights wlere incrementally placed in <br />the catch bucket during the calibration routine. After each <br />weight was centered in the bucket, the gage's bucket was tapped <br />and the chart drive cylinder was manually rotated slightly to <br />record the pen's trace on the chart. This was done for each <br />increment from 0 through 12 inches. The procedure was then <br />reversed~ each of the weights from 12 through 0 inches was <br />removed. Table 1 lists the deviations of each gage from the <br />respective chart inch levels. The calibration checks recorded <br />near the midpoint of the tests are also noted for a single <br />traverse range for each respective gage. <br /> <br />After the calibration was complet:ed, the gages and chart <br />drives were considered ready for test exercises. A calibration <br />weight (823.6 g) was pl aced in the cEmter of the catch bucket to <br />position the gage's pen arm at an opElrating range that might be <br />expected under field conditions. Thi.s simulated the weight of an <br />evapora tion suppressant/antifreeze charge that would be used <br />during winter field operations and would bring the initial level <br />of the gage above 0 inches. This procedure also kept the gage <br />from bottoming out on the platform movement stop screws. If the <br />system were to deviate significantly from the zero calibration <br />level, it is possible that considerable flow could enter the <br />catch bucket while resting on the stop screw, and not be detected <br />by the weighing mechanism. <br /> <br />After the calibration weight was placed in the catch bucket, <br />a second smaller catch beaker was placed on top of the weight <br />within the bucket to receive the flow from the IV tube. This <br />beaker, with an evaporation suppressant added, was weighed before <br />placement. The volume of evaporation suppressant was <br />approximately 10 cm3 and generally weighed nearly 8.2 g <br />(equivalent to 0.01 inch of precipitation). Texaco aircraft <br />hydraulic oil BB (petroleum base) was used for an evaporation <br />suppressant. The small catch beaker 'was used to allow for <br />convenient weighing of the total flow catch after each test. In <br />addi tion, with a smaller beaker, the is urface area of the 1 iquid <br />was reduced. This required less evaporation suppressant and <br />decreased the opportuni ty for evaporation. <br /> <br />5 <br />