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$ pwd<Enter> /home/quixoted $ cat .bashrc # .bashrc # User specific aliases and functions # Source global definitions if [ -f /etc/bashrc ]; then . /etc/bashrc fi # Begin aliases written by Quixote de La Mancha # Number 1 - Alias similar to old DOS command; written on July 23 alias dir-p= ls -l | less # End of aliases written by Quixote de La Mancha

Satellite constellations with intermittent coverage are generally useful for specific communication applications such as store-and-forward messagery or short voice transmission. Non-permanent coverage occurs only for non-geostationary orbits and when there are less satellites than the minimum number required for continuous coverage (see section 6.1.5.2), or when their number is large enough but when their relative placement is not optimized. A worst case is achieved with a constellation reduced to only one satellite. Depending on the altitude and the minimum elevation angle, typical average gaps in low-Earth orbits range from about 10 hours at 5 elevation and mid-latitudes with one satellite, to less than one hour with four satellites and about one half hour with six satellites. More quantified results require precise definitions of the zones of interest and of the constraints, together with specific numerical simulations. Generally, the constellations that are optimal for permanent coverage are not optimal for non-permanent coverage, but they generally provide fairly good initial conditions for the optimization process.

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This launch system was modified from earlier USSR large lift vehicles and is presently manufactured in the Ukraine by NPO Yuznoye. It is capable of lifting 4 300 kgs into a GTO. In a joint venture with Boeing (United States) and Kvaerner (Norway), the Sea Launch Company plans to increase this capability to 5 400 kgs by launching the Zenit from a modified ocean oil platform located on the equator. A schematic of the Zenit system in shown in Figure 6.40 with a sketch of the ocean platform under development by the Sea Launch Company's joint venture programme. With regard to other systems mentioned in this section, the reader is advised to seek out information from the organizations mentioned above for up-to-date information. Figure 6.35 Figure 6.36 Figure 6.37 Figure 6.38 Figure 6.39 Figure 6.40 Figure 6.41 Schematic of Ariane 5 launch system Atlas launch system design Growth of Delta family of launch systems with schematics of "Med-Lite" launchers History of Japanese launch systems Expanded view of Proton D-1 launch system showing major hardware components Schematic of Sea launch platform and Zenit 3SL launcher Long March Series of launch vehicles

The STYLE attribute should be used only if the other style methods cannot achieve the preferred style effects. The inline use of style only affects the associated tag. Therefore, it is not an optimal method to be used. There is another way to use inline styling by using the <SPAN> tag. This tag is used to apply style to selected portions of content in a tag. Consider that you want to develop a style that will highlight 257

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// Vanilla option (no discrete dividends, no barriers) on a single asset class VanillaOption : public Option { public: VanillaOption() { } VanillaOption(double price, double strike, double rate, double div, double vol, double T,

The formula in cell B2, which follows, returns the address of the cell in the Data range that contains the Target value:

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Grouping option Agglomerative hierarchical clustering k means clustering Fuzzy k means clustering Associative rules Decision trees

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in the wholesale can produce electricity for $044 (per kilowatthour) In the best of hypotheses with a reduction of 50% in stack cost, an improvement of 100% in the performance, and a hydrogen generation cost of $012 per gigajoule, FCPSs could supply energy at $023 (per kilowatthour) Commercial and manufacturing investment has been concentrated in three areas: (1) the development of a 5-kW reformer to be integrated with a fuel cell stack tolerant to fuel reforming; (2) commercially available fuel cells that operate with pure hydrogen and are integrated with electric vehicles, and (3) diffusion and training in the manufacture, production, and use of fuel cells For small- and medium-energy systems, the present state of the art seems to point toward the establishment to two already advanced technologies: proton exchange membrane and solid oxide fuel cells Therefore, this chapter concentrates next on those two technologies 7.

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