User:Rush1970/Heat shield

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added info about solr probe

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Revision as of 20:17, 30 April 2024
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In modern vehicles, passive cooling can be found as [[reinforced carbon–carbon]] material instead of metal. This material constitutes the thermal protection system of the nose and the front edges of the Space Shuttle and was proposed for the vehicle [[Lockheed Martin X-33|X-33]]. [[Carbon]] is the most refractory material known with a sublimation temperature (for [[graphite]]) of 3825&nbsp;°C. These characteristics make it a material particularly suitable for [[passive cooling]], but with the disadvantage of being very expensive and fragile. Some spacecraft also use a heat shield (in the conventional automotive sense) to protect fuel tanks and equipment from the heat produced by a large [[rocket engine]]. Such shields were used on the Apollo [[Apollo Command/Service Module#Service Module (SM)|Service Module]] and [[Apollo Lunar Module|Lunar Module]] descent stage.[[File:Gemini heat shield.jpg|thumb|Example of Ablative Heat Shield used for Gemini Missions]]In modern vehicles, passive cooling can be found as [[reinforced carbon–carbon]] material instead of metal. This material constitutes the thermal protection system of the nose and the front edges of the Space Shuttle and was proposed for the vehicle [[Lockheed Martin X-33|X-33]]. [[Carbon]] is the most refractory material known with a sublimation temperature (for [[graphite]]) of 3825&nbsp;°C. These characteristics make it a material particularly suitable for [[passive cooling]], but with the disadvantage of being very expensive and fragile. Some spacecraft also use a heat shield (in the conventional automotive sense) to protect fuel tanks and equipment from the heat produced by a large [[rocket engine]]. Such shields were used on the Apollo [[Apollo Command/Service Module#Service Module (SM)|Service Module]] and [[Apollo Lunar Module|Lunar Module]] descent stage. '''The [[Parker Solar Probe]] , designed to enter the corona of the Sun, experiences a surface temperature of 2,500 °F.'''<ref>{{Cite web |date=2018-07-05 |title=Cutting-Edge Heat Shield Installed on NASA’s Parker Solar Probe - NASA |url=https://www.nasa.gov/centers-and-fa...shield-installed-on-nasas-parker-solar-probe/ |access-date=2024-04-30 |language=en-US}}</ref> '''To withstand this temperature without damage to its body or instruments, the spacecraft uses a carbon-carbon ceramic with a layer of carbon foam in between as a heat shield.'''<ref>{{Cite web |last=Grossi |first=Stefano |title=Parker Solar Probe Heat Shield |url=https://ultramet.com/parker-solar-probe-heat-shield/ |access-date=2024-04-30 |website=Ultramet |language=en-US}}</ref>[[File:Gemini heat shield.jpg|thumb|Example of Ablative Heat Shield used for Gemini Missions]]
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