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Atmospheric re-entry

Due to their unique properties, a large number of groups all over the world are working in the area of CNTs for diverse applications and the most important are development and fabrication of sensors and thermal protection for atmospheric re-entry of space vehicles. Gas and glucose sensors based on CNTs have been developed. Some American researchers have recently claimed that they have developed CNT-based sensors for the detection of chemical warfare agents [80]. [Pg.394]

F. Monteverde and R. Savino Stability of ultra-high-temperature ZrB2-SiC ceramics under simulated atmospheric re-entry conditions. Journal of the European Ceramic Society 27,4797-4805 (2007). [Pg.135]

Carbon-carbon coating (depositing ceramic materials is possible in order to manufacture a nanostructured thermal barrier useful for aerospace vehicles during the atmosphere re-entry phase of a mission) (Fig. 6.21). [Pg.139]

Berton, B., Bacos, M. P, Demange, D., Lahaye, J. (1992). High-temperature oxidation of sihcon carbide in simulated atmospheric re-entry conditions. Journal of Materials Science, 27, 3206-3210. doi 10.1007/BF01116013. [Pg.268]

All equipment to be used at the field site should be calibrated at or near the field laboratory or field site prior to the application of the test substance (pesticide product). Most weather equipment will have been calibrated at the manufacturer and can be checked for functionality prior to the worker exposure/re-entry test by comparing weather readings from the nearest airport or National Oceanic and Atmospheric Administration (NOAA) weather reporting station with the weather readings compiled by the portable weather station. Hand-held weather instmments could also be checked with current weather reading from local airports or NOAA facilities. [Pg.994]

Literally removal , but applied particularly in space technology to the process of using up the frictional heat developed on re-entry of the vehicle into the Earth s atmosphere by degradation of the heat shield. Certain thermoplastics, thermosetting resins and polytetrafluoroethylene have been evaluated as ablative materials. [Pg.11]

Modern ceramic materials now include zirconium oxide (Zr02), titanium carbide (TiC), and silicon nitride (SiN). There are now many more uses of these new ceramic materials. For example, vehicle components such as ceramic bearings do not need lubrication - even at high speeds. In space technology, ceramic tiles protected the Space Shuttle from intense heat during its re-entry into the Earth s atmosphere. In the power supply industry, they are used as insulators due to the fact that they do not conduct electricity (Figure 3.39). [Pg.65]

The extent to which the molecules formed by recombination are in thermal equilibrium with the catalyst is of fundamental interest for the light it sheds on the nature of the interaction with the surface at the instant of reaction. It is also of practical interest, particularly in the use of thermal probes for the determination of atom concentrations, where the need to take account of factors influencing energy transfer processes has not always been recognised. Fresh interest in the phenomenon has been stimulated by the demands of space technology for information on surface heating due to recombination during re-entry into the earth s atmosphere. [Pg.211]

Suggestion 1 should always be practiced whenever possible. The re-entry of atmosphere into a vacuum system reintroduces copious amounts of moisture onto the vacuum system s walls and reintroduces gases back into the liquids within your system (oil and/or mercury). The next time the system is used, the walls will need to be re-dried and the liquids re-outgassed. Thus, a greater amount of time than would otherwise be necessary will be required the next time you wish to obtain a vacuum. This extra time will also place more wear and tear on your pumps and expose them to extra condensable vapors. [Pg.395]

However, at whole-body exposures at elevated temperatures (i.e., 95°F) and 35-97% relative humidity, the time to incapacitation was shortened. McNamara et al. reported that men may work without any signs of discomfort in an atmosphere where CS gradually accumulates, whereas these concentrations were intolerable to individuals entering the contaminated area from unexposed areas. Thus, it appears that adaptation develops gradually as the CS concentration increases. When the tolerant individual left the contaminated area for short periods of 10 to 30 min, the tolerance was lost, and re-entry into the contaminated areas resulted in intolerable irritation. Moreover, additional studies on human volunteers have documented the development of tolerance to CS. " ... [Pg.347]

The importance of carbon-fibre composite materials in the development of the space shuttle cannot be overemphasized. Reinforced carbon-carbon composites are used in the nose cone and wing leading edges to provide the resistance to thermal shock and stress required for re-entry into the Earth s atmosphere. Carbon-carbon composites are a particular group of carbon-fibre reinforced materials in which both the bulk material and fibres are carbon. The... [Pg.826]

It was established that under certain conditions of pesticide application after certain time periods (sometimes exceeding the re-entry period) products of pesticide degradation can enter the woridng zone atmosphere. The toxicity of these products was often higher than the original preparations. The probability of development of toxic mist under specific meteorological conditions was studied [9]. [Pg.292]

With re-entry vehicles and spaceplanes, the material resistance to extremes of temperature becomes a matter of major concern. When spacecraft dive into the Earth s atmosphere, aerodynamic surfaces are exposed to high thermal and mechanical loads maximum heat fluxes of the order of MW/nr, dynamic pressure, shear stress, acoustic vibrations and material degradation put the vehicles structures to a hard test. Payload and passenger survival is committed to the efficiency of the thermal protection system (TPS) which has to maintain the internal temperature within appropriate limits through various energy dissipating mechanisms. [Pg.41]

Phenolic laminates are also used in rocketry and space travel applications as heat shields during exit and re-entry into the earth s atmosphere. At very high temperatures, the surface burns away to leave a carbonaceous layer that glows and which is gradually sacrificed by ablation, protecting and insulating the under-surface for a considerable period. [Pg.210]

Detra, R.W., Hidalgo, H. (1961). Generalized heat transfer formulas and graphs for nose cone re-entry into the atmosphere. HRS Jowrwa/ 31(3) 318-321. [Pg.233]

Because of their high aromatic content, phenolic resins absorb a lot of heat for their degradation. This is why they are used as an ablative material in re-entry vehicles. When a space vehicle re-enters the earth s atmosphere, due to tremendous friction with air, a lot of heat is generated. Phenolic resins can absorb the heat at the cost of its degradation, and stops the vehicle from deteriorating as a result of the extremely high temperature. [Pg.72]


See other pages where Atmospheric re-entry is mentioned: [Pg.297]    [Pg.229]    [Pg.151]    [Pg.100]    [Pg.239]    [Pg.1160]    [Pg.79]    [Pg.11]    [Pg.83]    [Pg.83]    [Pg.87]    [Pg.125]    [Pg.355]    [Pg.655]    [Pg.297]    [Pg.229]    [Pg.151]    [Pg.100]    [Pg.239]    [Pg.1160]    [Pg.79]    [Pg.11]    [Pg.83]    [Pg.83]    [Pg.87]    [Pg.125]    [Pg.355]    [Pg.655]    [Pg.9]    [Pg.1190]    [Pg.16]    [Pg.6]    [Pg.12]    [Pg.266]    [Pg.112]    [Pg.284]    [Pg.245]    [Pg.904]    [Pg.23]    [Pg.41]    [Pg.954]    [Pg.119]    [Pg.216]    [Pg.1190]    [Pg.46]   
See also in sourсe #XX -- [ Pg.1153 , Pg.1160 , Pg.1161 ]




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Re-entry

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