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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 /> <br />1.5 <br /> <br />The highest priority in the program is to obtain the IMtJ and Ineteoro- <br />logical data, to various computations and building up data buffers. The <br />next priority is writing both position and meteorological dat~ on 1tape1 <br />lowest priority is assigned to the ~T display which is every 10 slaconds. <br /> <br />Tape drive failures are handled by a tape recovery routi.ne which re- <br />initializes the tape drive controller and displays a message on thla CRT <br />for the appropriate measures to be taken. As a result the operator will <br />manually restart the tape drive (if a severe failure occurs).. In illl other <br />cas.es the tape drive will automatically restart. <br /> <br />(b) The Pliqht Proqram: <br /> <br />The subcontract for the SP6 was awarded to North AmericcLn Weather <br />Consultants (NAWC) because of the familiarity of Richard Benner,. olE their <br />staff, with the SF 6 detecting equipment DRI rented from Dr. Ih'ian :r.amb, <br />Washington State University. <br /> <br />Richard Benner arrived at DRI 21 March 1985 and helped udjust and <br />install the instrument into the aircraft. He took charge of the ground <br />release of the SP6 gas. <br /> <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br /> <br />The initial flight was for 1.5 hours on 25 March 1985, :Ln the area of <br />Stead Airport. The SF 6 proved easy to de,tect at close range and the instru- <br />ments were all checked out. A number of aspects of the ordel~ in which the <br />graphical display is drawn needed to be changed so that the display was <br />readily visible at all times and the map was not concealed by the drum or <br />the pen block. These were then reprogrammed. Adjustment on the S:1:'6 <br />instrument for optimum performance proved to require patienc~a and skill, <br />and Benner I s participation proved essential to the success oj: the program. <br /> <br />The series of SF6 tracing flights which began just befo]~e the end of <br />the second quarter were completed at the beginning of the third qusrter. <br />The procedure worked well although a number of minor problenus had to be <br />solved before the equipment was entirely trouble free. <br /> <br />The graphical outputs from the 22 April 1985 flight are given as <br />Figures 1.2-1.6. These are direct reproductions of the real.-~ime plotter <br />output. Figure 1.2 shows the start of the flight at Stead Airport. The <br />strip charts at the top of the plot show altitude in kilometers with only <br />the fractional part plotted. When the tI'ace exceeds the limits, a unit of <br />1 kilometer is added or subtracted to keep the trace on scalIa, and the trace <br />annotated with the integer value which applies to the next section. Thus at <br />12:48 in Figure 1.2 the altitude begins a~t about 1.6 kilometlars (Stead Field <br />is 5060 or 1542 m). The SP6 output records volts from the instrument. It <br />starts at about 1.3 and is then adjusted to about 0.1 Volts. At 12:50 the <br />instrument is calibrated with a 25 ppt SE'6 sample and again ist 12: 54 . Some <br />adjustments were then made. Thus the sensitivity is about 50 ppb/Volt. <br />