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After I ve opened up a connection or two to my site s data sources, I m able to begin defining recordsets. Like connections, after recordsets are defined they are available sitewide, although they are generally applied to specific Web applications within the site. Therefore, I define a recordset only as it is needed in the creation of the page. It s very likely that the first couple of pages created for a site (such as the home page) are not dynamic, and no recordsets are needed. However, when it s time to define a recordset, you begin with the following steps: 1. Display the Bindings panel by choosing Window Bindings. 2. From the Bindings panel, click the Add button, and select Recordset from the dropdown list, as shown in Figure 2-4.

You want to take the fewest steps possible, with the simplest data and movie structure to achieve your predetermined goals Your navigation and its usability should also be considered The most simple and streamlined projects encounter fewer problems and errors along the way..

It is interesting to make a few direct comparisons of dielectric-wall Hall thrusters with metallic-wall TAL thrusters Similar discussions have appeared in the literature [1,3,31], often with conflicting opinions The basic plasma physics in the channel described above applies to both the dielectric-wall Hall thruster and the TAL The maximum electron temperature occurs in both thrusters near the channel exit in the region of strongest magnetic field where the Hall current is a maximum The different interaction of the thruster walls with this plasma determines many of the characteristics of the thruster, including life Dielectric-wall thrusters have a significant amount of their input power deposited as loss on the dielectric channel walls due to electron bombardment In the above example efficiency calculation, approximately 25% of the power going into the thruster was deposited on the channel walls.

Fig. 6-18: Push/Pull to make a building volume. Delete the extra lines on the face. Draw a line along the top length of the volume.

The metallic walls in TAL thrusters collect a smaller electron current because they are biased to cathode potential, and they also tend to have a small exposed area in poor contact with the plasma, which limits the amount of ion and power lost to these surfaces However, the anode is positioned very close to the high electron temperature region and receives a significant amount of power deposition in collecting the discharge current In the above example TAL efficiency calculation, over 20% of the power going into the thruster was deposited on the anode The deep channel in dielectric-wall Hall thrusters, with a low magnetic field strength and low electron temperature near the anode, tends to minimize the power deposition on the anode In the above simple example, only 1% of the thruster input power was deposited on the anode.

Using the Site Definition Wizard to define a new site is a quick, convenient way to get a site off the ground. In some cases, however, it is not complete. Depending on the site, you might have to use the Advanced tab of the Site Definition dialog box to specify additional site options, such as testing server details, cloaking, and so on.

Nevertheless, the anode is normally electrically isolated from the thruster body (and therefore thermally isolated), and so anode overheating is sometimes an issue, especially at high power density The anode in TAL thrusters can also have heating issues because the loading is much higher, even though the view factor for the anode to radiate its power out of the thruster is better than the deep channel in the insulting-wall configuration In addition, with the anode positioned physically close to the thruster exit in TALs, impurity deposition and material buildup problems can occur This has been an issue in ground testing of some TAL thrusters [29], where carbon deposition on the anode from back sputtering from the beam dump became significant over time TAL thrusters with deeper channels can be designed and operated [3].

The performance of the thruster is likely different in this configuration, and ion bombardment and sputtering of the metallic channel walls can become significant and affect the thruster life..

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Follow these steps to make incremental changes to the application: