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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 />- 29 - <br /> <br />signal paths. The first path is a pulse circuit which processes the pulse <br /> <br />signal from the ice crystal counter through a logarithmic amplifier and these <br /> <br />are then recorded on magnetic tape. The second path consists of an <br /> <br />integrating circuit which integrates the pulses and provides a visual <br /> <br />indication of the rate at which ice crystals are detected. This signal is <br />also recorded. <br />Initial airborne testing on the B-23 aircraft revealed the need for <br />extensive light shielding against the effects of ambient light chopping and <br />reflection from the aircraft propellers. Also, regulation of the power supply <br />to the arc lamp was found to be necessary. These problems were overcome and <br /> <br /> <br />subsequently several flights have been made with highly encouraging results. <br /> <br />The airborne tests have shown that this instrument can count ice <br /> <br /> <br />particles in clouds above a certain threshold size (yet to be determined <br /> <br />accurately) but that it does not "see" cloud droplets or even heavy rain. <br /> <br />The device therefore provides a rather dramatic improvement over previous <br /> <br />techniques for detecting ice particles in clouds. The most significant use <br /> <br />of the device so far has been as an aid in determining in real-time the <br /> <br />effects of artificial ice nuclei on increasing the concentrations of ice <br /> <br />particles in clouds. <br /> <br />1.3.5 Electrical Particle Counter <br /> <br />Preliminary work on the development of a device for counting cloud <br /> <br />particles from an aircraft by detecting the electrical charges they <br /> <br />communicate to a metal wire with which they collide was described by Mach <br /> <br />and Hobbs (1969). Further development and airborne testing of this device <br /> <br />has been carried out by Mr. W. Mach of 0UI' research group. <br />