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Last modified
7/28/2009 2:40:11 PM
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4/23/2008 1:57:54 PM
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Weather Modification
Title
The Use of Microwave Radiometry to Determine a Cloud Seeding Opportunity
Date
9/9/1982
Weather Modification - Doc Type
Report
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<br />SEPTEMBER 1982 <br /> <br />J. B. SNIDER AND D, ROTTNER <br /> <br />1287 <br /> <br />to make continuous observations of liquid water in <br />clouds, it was employed in the 1979-80 SCPP. <br />Briefly, the instrument simultaneously but indepen- <br />dently measures the absorption of a 28.5 GHz (wave- <br />length = 1.05 cm) microwave signal radiated by a <br />COMST AR communications satellite and the asso- <br />ciated microwave energy (brightness temperature) <br />emitted by liquid-bearing clouds that pass through <br />the propagation path. Independent, simultaneous <br />measurement of the two quantities is accomplished <br />using a unique design that allows coherent and in- <br />coherent reception with a single instrument. Opera- <br />tion in the two modes is made possible by means of <br />a switched-bandwidth receiver. When measuring the <br />signal from the satellite, a 200 kHz bandwidth is em- <br />ployed to obtain a high signal-to-noise ratio. How- <br />ever, when measuring the: incoherent, noise-like emis- <br />sion from the cloud, a 500 MHz bandwidth is used <br />so that the coherent signal from the satellite contrib- <br />utes a negligible amount t6 the total noise power re- <br />ceived by the radiometer. As a result, the two mea- <br />surements are independent. The receiving system <br />switches between the twOl bandwidths at a 40 Hz rate <br />so that the absorption and emission may be consid- <br />ered to be sampled simultaneously with respect to a <br />relatively slow-moving cloud in the propagation path. <br />The 40 Hz samples are averaged over 1 s intervals <br />before conversion to liquid values. <br />The two measurements are combined first to es- <br />timate an effective temperature of the liquid water in <br />the cloud, and second, to determine the absorption <br />coefficient which is a function of the liquid temper- <br />ature. Once the absorption coefficient has been de- <br />termined, the total amOlunt of liquid is calculated <br />from the measured absorption. <br />The effective temperature Tc of the liquid in the <br />cloud is calculated from <br /> <br />T = Tb <br />c 1 - exp(')' c/4.343) , <br /> <br />where Tb is the increase in emission, expressed as <br />brightness temperature, occurring when clouds pass <br />through the antenna beam, and 'Y c is the measured <br />absorption (in decibels) caused by the liquid-bearing <br />clouds. The effective cloud temperature is used to <br />compute the absorption coefficient a(T) in dB km-1 <br />g m-3, using a quadratic fit to the absorption-tem- <br />perature relationship reported by Gunn and East <br />(1954): <br /> <br />a(T) = 43.164 - 0.287Tc + 0.000482T/. (2) <br /> <br />Finally, L, the total amount of liquid per unit cross- <br />section (g m-2) along the propagation path, is cal- <br />culated from <br /> <br />L = i'c/a(T). <br /> <br />Since the radiometer does not provide information <br />on the dimensions of tht: cloud, it is convenient to <br /> <br />I... <br /> <br />(1) <br /> <br />normalize L to 1 km path length and to unit volume. <br />The quantity L then represents the total liquid (mm) <br />contained in the entire propagation path through the <br />cloud, regardless of its length. If the total path length <br />through the cloud is known from data obtained with <br />other sensors, an equivalent liquid water content <br />(LWC) in g m-3 can be obtained by dividing the total <br />liquid by the path length. For example, a total liquid <br />of 1 rom extending over a 1 km path length is equiv- <br />alent to a LWC of 1 g m-3. The threshold of liquid <br />detection for the system is -0.1 mm. <br />Because the radiometric method is based upon <br />sound, well-understood physical principles, the tech- <br />nique is believed to produce accurate measurements <br />ofliquid water in non-precipitating clouds containing <br />water droplets smaller than 100 Jlm. Indeed, a sys- <br />tematic comparison of cloud liquid measurements <br />made by two independent ground-based systems <br />showed consistent liquid values (within 0.28 mm rms) <br />for clouds observed simultaneously by the two sys- <br />tems (Snider et al., 1980b). <br />An example of the data output from the receiver- <br />radiometer is shown in the lower curve of Fig. 1. <br />Rainfall recorded at the Sheridan site using a weigh- <br />ing bucket raingage is plotted as vertical bars in the <br />upper curve; each bar represents the amount of rain <br />that has fallen in the previous 15 min. The rainfall <br />data are used as flags to indicate when radiometric <br />data may be suspect. Because raindrops are often <br />larger than 100 Jlm, Eq. (1) may not be valid during <br />rainfall. In addition, the larger attenuation in rain can <br />obscure absorption by water droplets in clouds. <br /> <br />3. Ailrborne instrumentation in the SCPP <br /> <br />Liquid water content and cloud microphysical data <br />were also measured by means of probes mounted on <br />a Beechcraft King Air 200 cloud physics aircraft <br />(N2UW) operated by the University of Wyoming. <br />Instruments carried on the aircraft for measurement <br />of L WC include a forward scattering spectrometer <br />probe (FSSP) and a Johnson-Williams (JW) hot-wire <br />probe. A series of imaging probes are available for <br />sensing ice particle size and concentration. A de- <br />celerator and slide sampler are used to capture ice <br />particles on oil-coated glass slides for later analysis. <br />Other instruments measure the velocity and position <br />of tht: aircraft, atmospheric turbulence, horizontal <br />and vertical winds, state parameters and ice nuclei. <br />A detailed description of the aircraft's instrumenta- <br />tion is given by Marwitz et al. (1978). <br />A second aircraft was employed in the 1979-80 <br />SCPP to dispense seeding materials and to observe <br />cloud characteristics. The second or "seeder" aircraft <br />was an Aero Commander Turboprop operated by <br />Aero Systems, Inc. of Boulder, CO; the aircraft had <br />the capability of dropping silver iodide (AgI) flares' <br />and dry ice (C02) pellets. A fuselage-mounted acetone <br />AgI gt:nerator was also available. <br /> <br />(3) <br />
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