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station keeping, and Fig. 8-1 shows the HughedBoeing patented [ I ] strategy for this function. Most modem satellites are three-axis stabilized with solar arrays that rotate to keep the cells pointed toward the Sun. From a thrust perspective, north-south station keeping is accomplished most efficiently if the thrusters point in the north and south directions. In geosynchronous orbit, the solar array axis of rotation points north and south, directly in the path of plumes from north-south station-keeping thrusters. The thruster energetic ion beam would impinge on the solar arrays and quickly damage them, dramatically shortening satellite life. The usual solution is to mount thrusters such that the resultant force is in the north-south direction, but each plume is at an angle with respect to the solar array axis. The larger the angle, the greater the thrust loss for station keeping, which leads to requirements for larger thrusters and more propellant mass; the smaller the angle, the greater the array damage, which reduces satellite life. This trade between north-south thrust efficiency and solar array life requires detailed knowledge of thruster plumes and their interactions. Electric thrusters used for primary propulsion, such as those on the National Aeronautics and Space Administration (NASA) Dawn mission to the asteroid belt, can also create issues associated with plume impact on the spacecraft solar

1. Add about 50 mL of starch indicator to the vessel. 2. Add suf cient iodine solution to the vessel to produce an intense black color. Note the quantity used. 3. With the agitator running at the desired speed, quickly incorporate sodium thiosulfate into the vessel at a rate approximately 2.5 times the quantity of iodine solution used. As mixing progresses, the liquid will clarify. 4. After each test, slowly add iodine solution until the neutral point is again reached, demonstrated by a hint of light blue appearing. The test can then be repeated. It should be noted that this technique must be used with care with solutions of CMC, which have a tendency to decolorize iodine solutions over time, albeit slowly.

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Incorporation of impurities in the crystals was a major concern that indicated higher impeller speeds but generated excessive nes, and the resulting poor ltration rates were a counterbalancing in uence on the determination of impeller speed. The two-level agitation rate scheme was a balance between these con icting factors, which gave passable purity, yield, and ltration rate. As in many high-impurity systems, however, the average particle size was small because of the need to operate at relatively high supersaturation to achieve practical growth rates, thereby incurring more nucleation than desired. The qualitative aspects of this dif cult crystallization provide examples of the trade-offs that are often encountered in development and scale-up.

A global network of professional FileMaker developers exists, many of whom provide and support complex applications for clients in a vast range of industries and in many countries of the world. FileMaker provides a certification program through a network of external test centers worldwide as a step toward the assurance of the knowledge and skill of professionals working in the field. Because FileMaker has been in use since 1985, professionals with extensive experience are available. For those located in Canada and the United States, FileMaker, Inc., publishes a FileMaker Resource Guide listing individuals and companies providing FileMaker-based solutions and consultancy services. The current edition is available online from the FileMaker Web site at www.filemaker. com/downloads/pdf/resource_guide.pdf.

The constant A, which is often about unity, depends on the impeller type. (see Table 11-7). Impellers with a high gas-handling capacity, such as hollow-blade disk designs, have the highest values. As will also be seen in Table 11-7, the exponent B varies considerably with impeller type but is about 0.4 for Rushton and pitched blade turbines. Figure 11-16 reproduces some results for a six-blade Rushton turbine working at various submergences and boil-up rates. In this case the constant A in eq. (11-12) is 0.74. A critical (CAg )crit (or Smcrit ) can be de ned as that value above which the power draw is essentially the same as when this impeller, is ungassed. For a Rushton impeller, this value is about 2.1 and values for other impellers are given

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