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<br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br /> <br />The specific observations involved will now be discussed in the same order. All the <br />instrumentation systems discussed are summarized in table 4.1 at the end of this subsection. <br />The relative locations of the systems are shown on figure 4, which represents an approximate <br />composite of the two proposed experimental areas. <br /> <br />4.6.1 Existence of excess SLW over the barrier <br /> <br />The existence of SLW over the mountain barrier will be monitored with two microwave <br />radiometers. One will monitor cloud conditions over the upwind side of the barrier where <br />orographic production of liquid is maximized (Huggins, 1992; Huggins et al., 1992:). The other <br />radiometer will be located near the centerline of the barrier top, to measure any excess SLW <br />just prior to its downward transport within the lee subsidence zone. Both radiometer sites will <br />be equipped with accurate tower-mounted sensors to measure air temp€!rature and <br />dewpoint/frostpoint temperature. These observations will indicate when the lower atmosphere <br />is saturated with respect to water and ice. <br /> <br />Liquid cloud (or at least ice saturation) would have to exist over one or both radiometers for <br />seeding potential to be present. Existence of SLW over the upwind radiometer but not over the <br />downwind unit might suggest that nature had converted all condensate to ice prior to the air <br />crossing the mountain range so that little seeding potential exists. This possibility villI be tested <br />during the direct detection experiments, by aircraft and surface observations. The downwind <br />radiometer would not likely detect SLW when none existed over the upwind instrument unless <br />individual convective cells were being transported across the barrier. <br /> <br />In addition to radiometer observations, SLW will be monitored by icing rate meters maintained <br />at some of the seeding sites and on towers on top the barriers. These units res.pond to the <br />buildup of ice fonned by the impact and freezing of supercooled cloud droplets. After ice <br />thickness reaches a preset limit, the small exposed sensing rod is briefly heated to shed its ice, <br />after which the unit is ready for another buildup cycle. The rate of cycling is proportional to the <br />SLW flux past the instrument. Wind will also be measured at the icing rate meter sites, and <br />accurate sensors will monitor whether the air is saturated with respect to ice so that at least <br />diffusional growth of ice crystals is possible. Periodic rawinsonde releases will provide further <br />evidence of saturated layers upwind of the mountain barriers. <br /> <br />Aircraft observations of SL W periodically will be made over the windward slopes, ~md over the <br />target area, during daytime direct detection seeding experiments. These measurements will be <br />made from about 300 m above highest nearby terrain to the top of the liquid water cloud. <br /> <br />4.6.2 Reliable production of seeding agents <br /> <br />Each AgI generator and liquid propane dispenser will be automatically monitored to check <br />proper operation. Flame temperature and solution flow will be measured at the AgI generators, <br />and the propane dispensers will use both a flow rate sensor and a temperature sensor to verify <br />vaporization of the liquid propane at the output nozzle. These observations will be transmitted <br />by radio to a central monitoring station. Frequent manual checking of remote-controlled units <br />will be accomplished until confidence is gained in their reliable operation. Sample generators <br />will be tested for ice nucleus effectiveness in a cloud simulation laboratory. <br /> <br />25 <br />