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Electrons temperature variation

The ions gain energy from the warmer electrons and lose energy to the colder neutrals. Below about 400 km, the ions strongly couple to the neutrals, and the ion temperature variation merely reflects the variation in the neutral temperature, which is not as dramatic as the electron temperature variation. Above 400 km, the ion temperature increases with altitude due primarily to the increased thermal coupling to the warm electrons there is also a small downward ion heat flow from high altitudes. Note that above 400 km, the ion temperature displays a very small variation from day to night. [Pg.182]

Figure 12. Variation of the plasma parameters of a CH4/H2 plasma with pressure, (a) Plasma potential, (b) Electron temperature, (c) Electron density. Reprinted with permission from [88], K. Okada et al., /. Vac. Sci. TechnoL, A 17, 721 (1999). 1999, American Institute of Physics. Figure 12. Variation of the plasma parameters of a CH4/H2 plasma with pressure, (a) Plasma potential, (b) Electron temperature, (c) Electron density. Reprinted with permission from [88], K. Okada et al., /. Vac. Sci. TechnoL, A 17, 721 (1999). 1999, American Institute of Physics.
Figure 14. Variation of the plasma parameters of a CH4/CO/H2 plasma with [CO] content, (a) Plasma potential, (b) Electron temperature, (c) Electron density. Figure 14. Variation of the plasma parameters of a CH4/CO/H2 plasma with [CO] content, (a) Plasma potential, (b) Electron temperature, (c) Electron density.
Fig. 3.21 Example of temperature variation as measured by MIMOS II temperature sensors on MER (i) inside the rover body at MIMOS electronics board (black curve), (ii) outside the rover, at the MIMOS II SH (green and red curves), which is at ambient Martian temperature (a) inside the sensor-head, at the reference absorber position (green), (b) outside the SH at the sample s contact plate (red). Temperatures at the two SH positions are nearly identical (difference less than 2 K). During data transmission between the rover and the Earth (or the relay satellite in Mars orbit) the instrument is switched off resulting in immediate small but noticeable temperature changes (see figure above)... Fig. 3.21 Example of temperature variation as measured by MIMOS II temperature sensors on MER (i) inside the rover body at MIMOS electronics board (black curve), (ii) outside the rover, at the MIMOS II SH (green and red curves), which is at ambient Martian temperature (a) inside the sensor-head, at the reference absorber position (green), (b) outside the SH at the sample s contact plate (red). Temperatures at the two SH positions are nearly identical (difference less than 2 K). During data transmission between the rover and the Earth (or the relay satellite in Mars orbit) the instrument is switched off resulting in immediate small but noticeable temperature changes (see figure above)...
Tong G., Christopher, D.M., Li, B. (2009). Numerical modelling of temperature variations in a Chinese solar greenhouse. Computers and Electronics in Agriculture, 68(1), 129-139. [Pg.241]

Figure 3. Variation of ion and electron temperatures with gas pressure in a plasma. Figure 3. Variation of ion and electron temperatures with gas pressure in a plasma.
So how does the IRMS get its stability Collector slits are several times the width of the ion beams. This gives a flat-topped peak shape (Fig 6) which makes the ion current intensive to drift. The main source of drift is temperature variation which both affects the electronic components used for mass selection and caused expansion and contraction of mechanical parts. Simultaneous measurement of ion beams using a double or triple collector is more precise than sequential measurement by mass scanning with a single detector. Finally, frequent comparison of sample gas under identical conditions also contributes to stability. Ion beam stability is more important than resolution for isotopic measurements. [Pg.160]

Figure 5. Model spectra of a naked neutron star. The emitted spectrum with electron-phonon damping accounted for and Tsurf = 106 K. Left panel uniform surface temperature right panel meridional temperature variation. The dashed line is the blackbody at Tsurf and the dash-dotted line the blackbody which best-fits the calculated spectrum in the 0.1-2 keV range. The two models shown in each panel are computed for a dipole field Bp = 5 x 1013 G (upper solid curve) and Bp = 3 x 1013 G (lower solid curve). The spectra are at the star surface and no red-shift correction has been applied. From Turolla, Zane and Drake (2004). Figure 5. Model spectra of a naked neutron star. The emitted spectrum with electron-phonon damping accounted for and Tsurf = 106 K. Left panel uniform surface temperature right panel meridional temperature variation. The dashed line is the blackbody at Tsurf and the dash-dotted line the blackbody which best-fits the calculated spectrum in the 0.1-2 keV range. The two models shown in each panel are computed for a dipole field Bp = 5 x 1013 G (upper solid curve) and Bp = 3 x 1013 G (lower solid curve). The spectra are at the star surface and no red-shift correction has been applied. From Turolla, Zane and Drake (2004).
Recognition of specific definite variables which are beyond anyone s control lying very close to the performance limit of an instrument, such as temperature variations, noise as well as drift from an electronic circuit, and vibrations caused to a building by heavy vehicular-traffic,... [Pg.74]

From the temperature variation of the equilibrium constant, thermodynamic parameters for the reaction were also obtained. The extent of formation of [Mo(CO)5l]" was found to be cation-dependent, and while equilibrium constants of 39 and 21 atm L moF were obtained for Bu4P and pyH+, none of the anionic iodide complex was observed for Na. Despite this variation, there seemed to be no correlation between the concentration of [Mo(CO)5l]" and the rate of the catalytic carbonylation reaction. It was proposed that [Mo(CO)5] and [Mo(CO)5l] are spectator species, with the catalysis being initiated by [Mo(CO)5]. Based on the in situ spectroscopic results and kinetic data, a catalytic mechanism was suggested, involving radicals formed by inner sphere electron transfer between EtI and [Mo(CO)5]. [Pg.131]

The mobilities of holes are always less than those of electrons that is fXh < Me- In silicon and germanium, the ratio [ie/[ih is approximately three and two, respectively (see Table 6.2). Since the mobilities change only slightly as compared to the change of the charge carrier densities with temperature, the temperature variation of conductivity for an intrinsic semiconductor is similar to that of charge carrier density. [Pg.552]

Metal Oxide-Polymer Thermistors. The variation of electrical properties with temperature heretofore described can be used to tremendous advantage. These so-called thermoelectric effects are commonly used in the operation of electronic temperature measuring devices such as thermocouples, thermistors, and resistance-temperature detectors (RTDs). A thermocouple consists of two dissimilar metals joined at one end. As one end of the thermocouple is heated or cooled, electrons diffuse toward... [Pg.594]

Ambient temperature variations will affect the accuracy and reliability of temperature detection instrumentation. Variations in ambient temperature can directly affect the resistance of components in a bridge circuit and the resistance of the reference junction for a thermocouple. In addition, ambient temperature variations can affect the calibration of electric/electronic equipment. The effects of temperature variations are reduced by the design of the circuitry and by maintaining the temperature detection instrumentation in the proper environment. [Pg.27]

The temperature dependence of k, was investigated and reported in Ref. [266], To obtain low-temperature data, samples were prepared in a 50% glycerol-water mixture. Figure 33 presents the temperature variation of k,. One can see from this Fig. that the electron transfer rate falls smoothly from the room temperature value to a non-zero value, kt = 9 + 4 s 1, which does not vary further from 170 down to 77 K. Data in the temperature-dependent region (T > 253 K) give the value Ea 2 kcal mol 1 for the Arrhenius activation energy. [Pg.69]


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