Difference between revisions of "Ablating Material"
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| − | + | An '''Ablating Material''' is a material, especially a coating material, designed to provide thermal protection to a body in a fluid stream through loss of mass. | |
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| − | thermal protection to a body in a fluid stream through loss of | + | Ablating materials are used on the surfaces of some reentry vehicles to absorb heat by removal of mass, thus blocking the transfer of heat to the rest of the vehicle and maintaining temperatures within design limits. Ablating materials absorb heat by increasing in temperature and changing in chemical or physical state. The heat is carried away from the surface by a loss of mass (liquid or vapor). The departing mass also blocks part of the convective heat transfer to the remaining material in the same manner as [[Transpiration Cooling|transpiration cooling]]. |
| − | mass. | ||
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| − | vehicles to absorb heat by removal of mass, thus blocking the | ||
| − | transfer of heat to the rest of the vehicle and maintaining temperatures | ||
| − | within design limits. Ablating materials absorb heat by increasing | ||
| − | in temperature and changing in chemical or physical state. The | ||
| − | heat is carried away from the surface by a loss of mass (liquid | ||
| − | or vapor). The departing mass also blocks part of the convective | ||
| − | heat transfer to the remaining material in the same manner as | ||
| − | [[Transpiration Cooling|transpiration cooling]]. | ||
==References== | ==References== | ||
''This article is based on NASA's [[NASA SP-7|Dictionary of Technical Terms for Aerospace Use]]'' | ''This article is based on NASA's [[NASA SP-7|Dictionary of Technical Terms for Aerospace Use]]'' | ||
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| − | [[Category | + | [[Category:NASA SP-7]] |
| + | [[Category:Spacecraft Construction]] | ||
| + | [[Category:Re-entry]] | ||
| + | [[Category:Rocketry]] | ||
Revision as of 13:46, 20 March 2007
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An Ablating Material is a material, especially a coating material, designed to provide thermal protection to a body in a fluid stream through loss of mass.
Ablating materials are used on the surfaces of some reentry vehicles to absorb heat by removal of mass, thus blocking the transfer of heat to the rest of the vehicle and maintaining temperatures within design limits. Ablating materials absorb heat by increasing in temperature and changing in chemical or physical state. The heat is carried away from the surface by a loss of mass (liquid or vapor). The departing mass also blocks part of the convective heat transfer to the remaining material in the same manner as transpiration cooling.
References
This article is based on NASA's Dictionary of Technical Terms for Aerospace Use
