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First-flight losses

Figure 8 shows the relatively simple powder diffraction pattern of polycrystalline silicon, measured by time-of-flight neutron diffraction. Each allowed Bragg peak for the crystal structure is observed as a sharp peak in the diffraction pattern. A fundamental difference between single crystal and powder diffraction is that the single crystal diffraction pattern has the full directional information described by Equation [28], whereas for the powder diffraction pattern this information has been collapsed down into a onedimensional function. This difference has two important consequences firstly, the loss of directional information makes it very much more difficult to... [Pg.341]

It is well know that melting occurs more rapidly if there is a positive pressure at the end of the transition zone. If Film B is considered to be large and if the pressure in the melt Film C is essentially zero at the trailing flight, a first order approximation of this pressure effect can be achieved by adding a pressure dissipation term to the rate of material loss in the y direction of the solid surface adjacent to the Film C ... [Pg.732]

Viton was the first of these important systems to be developed as an elastomer suitable for use in aggressive environments. Consequently, this and related materials have made a particularly important contribution to the development of supersonic and space flight. The raw copolymer itself is quite unstable to the loss of hydrogen fluoride and the final product is a result of cross-linking and curing processes. These techniques have been the basis of much study over many years [223]. [Pg.205]

To see more fringes we have to increase the coherence length and therefore decrease the velocity spread. For this purpose we employ a mechanical velocity selector, as shown after the oven in Fig. 1. It consists of four slotted disks that rotate around a common axis. The first disk chops the fullerene beam. Only those molecules are transmitted which traverse the distance from one disk to the next in the same time that the disks rotate from one open slot to the next. Although two disks would suffice for this purpose, the additional disks decrease the velocity spread even further and help to eliminate velocity sidebands. By varying the rotation frequency of the selector, the desired velocity class of the transmitted molecules can be adjusted. To measure the time of flight distribution we chopped the fullerene beam with the chopper right behind the source (see Fig. 1). The selection is of course accompanied by a significant loss in count rate, but we can still retain about 7% of the unselected molecules. [Pg.337]

The first evidence of secondary dissociation appears in the time-of-flight spectrum of m/e = 54. This ion corresponds to a loss of a total of three NOj groups from TNAZ. Since the ion giving the m/e = 100 differs from the m/e = 54 ion by one NO2 group, it is reasonable to expect that the faster m/e = 5A signal is due to secondary decomposition of the heavier fragment (produced by Reaction 1) via toss of NO2... [Pg.47]

FADEC systems govern the thrust control of engines. Therefore, the certification requirements for the application of TLD to FADEC systems require that the Loss of Thrust Control (LOTC) rates related to those systems must meet certain requirements. There are two basic requirements. The first of these is that the average system LOTC rate must not exceed 10 failures per 10 flight hours. This limit was established since this... [Pg.667]

STS-112 October 7, 2002 Sixth known left bipod ramp foam loss. First time major debris event not assigned an in-flight anomaly. External tank project was assigned an Action. Not closed out until after STS-113 and STS-107. [Pg.15]


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See also in sourсe #XX -- [ Pg.151 , Pg.647 ]




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First loss

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