[[Spacecraft]] that land on a [[planet]] with an [[atmosphere]], such as [[Earth]], [[Mars]], and [[Venus]], currently do so by entering the atmosphere at high speeds, depending on [[air resistance]] rather than rocket power to slow them down. A side effect of this method of atmospheric re-entry is [[aerodynamic heating]], which can be highly destructive to the structure of an unprotected or faulty spacecraft.<ref>{{cite web |url=http://www.phys.ttu.edu/~cmyles/Phys4304/Papers/Dynamics-of-Atmospheric-Rentry.doc |title=Dynamics of Atmospheric Rentry |access-date=2016-08-23 |archive-date=2018-07-08 |archive-url=https://web.archive.org/web/20180708015436/http://www.phys.ttu.edu/~cmyles/Phys4304/Papers/Dynamics-of-Atmospheric-Rentry.doc |url-status=live }}</ref> An aerodynamic heat shield consists of a protective layer of special materials to dissipate the heat. Two basic types of aerodynamic heat shield have been used:
[[Spacecraft]] that land on a [[planet]] with an [[atmosphere]], such as [[Earth]], [[Mars]], and [[Venus]], currently do so by entering the atmosphere at high speeds, depending on [[air resistance]] rather than rocket power to slow them down. A side effect of this method of atmospheric re-entry is [[aerodynamic heating]], which can be highly destructive to the structure of an unprotected or faulty spacecraft.<ref>{{cite web |url=http://www.phys.ttu.edu/~cmyles/Phys4304/Papers/Dynamics-of-Atmospheric-Rentry.doc |title=Dynamics of Atmospheric Rentry |access-date=2016-08-23 |archive-date=2018-07-08 |archive-url=https://web.archive.org/web/20180708015436/http://www.phys.ttu.edu/~cmyles/Phys4304/Papers/Dynamics-of-Atmospheric-Rentry.doc |url-status=live }}</ref> An aerodynamic heat shield consists of a protective layer of special materials to dissipate the heat. Two basic types of aerodynamic heat shield have been used:
*An [[ablative heat shield]] consists of a layer of plastic resin, the outer surface of which is heated to a gas, which then carries the heat away by [[convection]]. Such shields were used on the [[Project Mercury#Spacecraft|Mercury]], [[Project Gemini#Spacecraft|Gemini]], and [[Apollo (spacecraft)|Apollo]] spacecraft, and are currently used by the [[SpaceX Dragon 2]] spacecraft and the [[Orion (spacecraft)|Orion]] spacecraft.
*An [[ablative heat shield]] consists of a layer of plastic resin, the outer surface of which is heated to a gas, which then carries the heat away by [[convection]]. Such shields were used on the [[Project Mercury#Spacecraft|Mercury]], [[Project Gemini#Spacecraft|Gemini]], and [[Apollo (spacecraft)|Apollo]] spacecraft, and are currently used by the [[SpaceX Dragon 2]] spacecraft and the [[Orion (spacecraft)|Orion]] spacecraft.
**The Russian [[Vostok 1]], the first manned spacecraft, used ablative heat shielding made from asbestos fabric in resin.<ref>{{Cite web |title=Бобков В. Космический корабль "Восток". |url=https://epizodsspace.airbase.ru/bibl/k-r/1991/4-5vostok.html |access-date=2024-03-22 |website=epizodsspace.airbase.ru}}</ref> The succeeding Mercury and Gemini missions both used fiber glass in the resin, while the Apollo spacecraft using a quartz fiber reinforced resin.<ref name=":0">{{Cite journal |last=Venkatapathy |first=Ethiraj |date=2019-10-21 |title=Ablators - From Apollo to Future Missions to Moon, Mars and Beyond |url=https://ntrs.nasa.gov/citations/20190032222 |language=en}}</ref> The first use of a super-light ablator(SLA) spacecraft purposes was for the [[Viking program|Viking Landers]] in 1976.<ref name=":03">{{Cite journal |last=Venkatapathy |first=Ethiraj |date=2019-10-21 |title=Ablators - From Apollo to Future Missions to Moon, Mars and Beyond |url=https://ntrs.nasa.gov/citations/20190032222 |language=en}}</ref> SLA would also be utilized for the [[Mars Pathfinder|Pathfinder mission]].<ref name=":04">{{Cite journal |last=Venkatapathy |first=Ethiraj |date=2019-10-21 |title=Ablators - From Apollo to Future Missions to Moon, Mars and Beyond |url=https://ntrs.nasa.gov/citations/20190032222 |language=en}}</ref>
**The Russian [[Vostok 1]], the first manned spacecraft, used ablative heat shielding made from asbestos fabric in resin.<ref>{{Cite web |title=Бобков В. Космический корабль "Восток". |url=https://epizodsspace.airbase.ru/bibl/k-r/1991/4-5vostok.html |access-date=2024-03-22 |website=epizodsspace.airbase.ru}}</ref> The succeeding Mercury and Gemini missions both used fiber glass in the resin, while the Apollo spacecraft using a quartz fiber reinforced resin.<ref name=":0">{{Cite journal |last=Venkatapathy |first=Ethiraj |date=2019-10-21 |title=Ablators - From Apollo to Future Missions to Moon, Mars and Beyond |url=https://ntrs.nasa.gov/citations/20190032222 |language=en}}</ref> The first use of a super-light ablator(SLA) spacecraft purposes was for the [[Viking program|Viking Landers]] in 1976.<ref name=":03">{{Cite journal |last=Venkatapathy |first=Ethiraj |date=2019-10-21 |title=Ablators - From Apollo to Future Missions to Moon, Mars and Beyond |url=https://ntrs.nasa.gov/citations/20190032222 |language=en}}</ref> SLA would also be utilized for the [[Mars Pathfinder|Pathfinder mission]].<ref name=":04">{{Cite journal |last=Venkatapathy |first=Ethiraj |date=2019-10-21 |title=Ablators - From Apollo to Future Missions to Moon, Mars and Beyond |url=https://ntrs.nasa.gov/citations/20190032222 |language=en}}</ref> Phenolic impregnated carbon ablators(PICA) was used for the Stardust mission launched in 1999.<ref name=":05">{{Cite journal |last=Venkatapathy |first=Ethiraj |date=2019-10-21 |title=Ablators - From Apollo to Future Missions to Moon, Mars and Beyond |url=https://ntrs.nasa.gov/citations/20190032222 |language=en}}</ref>
*A [[Atmospheric entry#Thermal soak|thermal soak heat shield]] uses an insulating material to absorb and radiate the heat away from the spacecraft structure. This type was used on the [[Space Shuttle]], with the intent for the shield to be reused with minimal refurbishment in between launches.<ref name=":02">{{Cite book |url=https://www.worldcat.org/title/698332185 |title=Wings in orbit: scientific and engineering legacies of the space shuttle, 1971-2010 |date=2010 |publisher=National Aeronautics and Space Administration |isbn=978-0-16-086846-7 |editor-last=Hale |editor-first=Wayne |series=NASA/SP |location=Washington, D.C. |oclc=698332185 |editor-last2=Lane |editor-first2=Helen W. |editor-last3=United States}}</ref> The heat shield on the space shuttle consisted of [[Space Shuttle thermal protection system#Materials|ceramic or composite tiles]] over most of the vehicle surface, with [[reinforced carbon-carbon]] material on the highest [[heat load]] points (the nose and wing leading edges).<ref>{{Cite journal |last1=Meechan |first1=C. J. |last2=Miles |first2=F. |last3=Ledsome |first3=C. |last4=Fraser |first4=D. O. |last5=Whitehouse |first5=D. |date=1984 |title=The Space Shuttle System [and Discussion] |url=https://www.jstor.org/stable/37389 |journal=Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences |volume=312 |issue=1519 |pages=89–102 |doi=10.1098/rsta.1984.0053 |jstor=37389 |issn=0080-4614}}</ref> Damage to this material on the left wing caused the 2003 [[Space Shuttle Columbia disaster|Space Shuttle ''Columbia'' disaster]].<ref>{{Cite book |last1=Leinbach |first1=Micheal D. |title=Bringing Columbia Home: The Untold True Story of a Lost Space Shuttle and Her Crew |last2=Ward |first2=Jonathan H. |publisher=Arcade Publishing |year=2020 |isbn=9781948924610 |location=New York, NY |pages=229–234}}</ref>
*A [[Atmospheric entry#Thermal soak|thermal soak heat shield]] uses an insulating material to absorb and radiate the heat away from the spacecraft structure. This type was used on the [[Space Shuttle]], with the intent for the shield to be reused with minimal refurbishment in between launches.<ref name=":02">{{Cite book |url=https://www.worldcat.org/title/698332185 |title=Wings in orbit: scientific and engineering legacies of the space shuttle, 1971-2010 |date=2010 |publisher=National Aeronautics and Space Administration |isbn=978-0-16-086846-7 |editor-last=Hale |editor-first=Wayne |series=NASA/SP |location=Washington, D.C. |oclc=698332185 |editor-last2=Lane |editor-first2=Helen W. |editor-last3=United States}}</ref> The heat shield on the space shuttle consisted of [[Space Shuttle thermal protection system#Materials|ceramic or composite tiles]] over most of the vehicle surface, with [[reinforced carbon-carbon]] material on the highest [[heat load]] points (the nose and wing leading edges).<ref>{{Cite journal |last1=Meechan |first1=C. J. |last2=Miles |first2=F. |last3=Ledsome |first3=C. |last4=Fraser |first4=D. O. |last5=Whitehouse |first5=D. |date=1984 |title=The Space Shuttle System [and Discussion] |url=https://www.jstor.org/stable/37389 |journal=Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences |volume=312 |issue=1519 |pages=89–102 |doi=10.1098/rsta.1984.0053 |jstor=37389 |issn=0080-4614}}</ref> Damage to this material on the left wing caused the 2003 [[Space Shuttle Columbia disaster|Space Shuttle ''Columbia'' disaster]].<ref>{{Cite book |last1=Leinbach |first1=Micheal D. |title=Bringing Columbia Home: The Untold True Story of a Lost Space Shuttle and Her Crew |last2=Ward |first2=Jonathan H. |publisher=Arcade Publishing |year=2020 |isbn=9781948924610 |location=New York, NY |pages=229–234}}</ref>
In engineering, a heat shield is a component designed to protect an object or a human operator from being burnt or overheated by dissipating, reflecting, and/or absorbing heat. The term is most often used in reference to exhaust heat management and to systems for dissipating frictional heat. Heat shields are used most commonly in automotive and aerospace.
Principles of operation
Heat shields protect structures from extreme temperatures and thermal gradients by two primary mechanisms. Thermal insulation and radiative cooling, respectively isolate the underlying structure from high external surface temperatures, while emitting heat outwards through thermal radiation. To achieve good functionality the three attributes required of a heat shield are low thermal conductivity (high thermal resistance), high emissivity, and good thermal stability (refractoriness).[1] Porous ceramics with high emissivity coatings (HECs) are often employed to address these three characteristics, owing to the good thermal stability of ceramics, the thermal insulation of porous materials and the good radiative cooling effects offered by HECs.
Due to the large amounts of heat given off by internal combustion engines,[2] heat shields are used on most engines to protect components and bodywork from heat damage. As well as protection, effective heat shields can give a performance benefit by reducing engine bay temperatures, therefore reducing the temperature of the air entering the engine.[3] Heat shields vary widely in price, but most are easy to fit, usually by stainless steel clips, high temperature tape or specially designed metal cable ties. There are three main types of automotive heat shield:
An example of a steel heat shield on a BMW E series engineRigid heat shields have until recently commonly been made from solid steel,[4] but are now often made from aluminum. Some high-end rigid heat shields are made out of either aluminum, gold or composite, with most examples including a ceramic coating to provide a thermal barrier, which improves heat insulation.
The flexible heat shield are normally made from thin aluminum or gold sheeting, most commonly sold either flat or in a roll. These heat shields are often bent by hand by the installer. High performance flexible heat shields sometimes include extras, such as ceramic insulation applied via plasma spraying. Another common tactic in flexible heat shields is using exotic composite materials to improve thermal insulation and shave weight. These latest products are commonplace in top-end motorsports such as Formula 1.
An example of an aluminum heat shield on the Toyota Celica ST205Textile heat shields, (also known as heat wraps), are used to insulate various exhaust components by trapping the heat emitted by the exhaust inside the exhaust pipe, rather than allowing the immense heat from these components to radiate within the engine bay. These wraps are most common in motorcycle exhaust pipes.
Heat shields are often fitted by both amateur and professional personnel during the optimization phase of engine tuning. Heat shields are also used to cool engine mount vents. When a vehicle is at higher speed there is enough ram air to cool the under the hood engine compartment, but when the vehicle is moving at lower speeds or climbing a gradient there is a need of insulating the engine heat to get transferred to other parts around it, e.g. Engine Mounts. With the help of proper thermal analysis and use of heat shields, the engine mount vents can be optimized for the best performances.[5]
Aircraft
Some aircraft at high speed, such as the Concorde and SR-71 Blackbird, must be designed considering similar, but lower, overheating to what occurs in spacecraft. In the case of the Concorde the aluminum nose can reach a maximum operating temperature of 127 °C (which is 180 °C higher than the ambient air outside which is below zero); the metallurgical consequences associated with the peak temperature were a significant factor in determining the maximum aircraft speed.
Recently new materials have been developed that could be superior to RCC. The prototype SHARP (Slender Hypervelocity Aerothermodynamic Research Probe) is based on ultra-high temperature ceramics such as zirconium diboride (ZrB2) and hafnium diboride (HfB2).[6] The thermal protection system based on these materials would allow to reach a speed of Mach number 7 at sea level, Mach 11 at 35000 meters and significant improvements for vehicles designed for hypersonic speed. The materials used have thermal protection characteristics in a temperature range from 0 °C to + 2000 °C, with melting point at over 3500 °C. They are also structurally more resistant than RCC, so they do not require additional reinforcements, and are very efficient in re-irradiating the absorbed heat. NASA funded (and subsequently discontinued) a research and development program in 2001 for testing this protection system through the University of Montana.[7][8]
Apollo 12 capsule's ablative heat shield (after use) on display at the Virginia Air and Space CenterThermal soak aerodynamic heat shield used on the Space Shuttle
Spacecraft that land on a planet with an atmosphere, such as Earth, Mars, and Venus, currently do so by entering the atmosphere at high speeds, depending on air resistance rather than rocket power to slow them down. A side effect of this method of atmospheric re-entry is aerodynamic heating, which can be highly destructive to the structure of an unprotected or faulty spacecraft.[10] An aerodynamic heat shield consists of a protective layer of special materials to dissipate the heat. Two basic types of aerodynamic heat shield have been used:
An ablative heat shield consists of a layer of plastic resin, the outer surface of which is heated to a gas, which then carries the heat away by convection. Such shields were used on the Mercury, Gemini, and Apollo spacecraft, and are currently used by the SpaceX Dragon 2 spacecraft and the Orion spacecraft.
The Russian Vostok 1, the first manned spacecraft, used ablative heat shielding made from asbestos fabric in resin.[11] The succeeding Mercury and Gemini missions both used fiber glass in the resin, while the Apollo spacecraft using a quartz fiber reinforced resin.[12] The first use of a super-light ablator(SLA) spacecraft purposes was for the Viking Landers in 1976.[13] SLA would also be utilized for the Pathfinder mission.[14] Phenolic impregnated carbon ablators(PICA) was used for the Stardust mission launched in 1999.[15]
A thermal soak heat shield uses an insulating material to absorb and radiate the heat away from the spacecraft structure. This type was used on the Space Shuttle, with the intent for the shield to be reused with minimal refurbishment in between launches.[16] The heat shield on the space shuttle consisted of ceramic or composite tiles over most of the vehicle surface, with reinforced carbon-carbon material on the highest heat load points (the nose and wing leading edges).[17] Damage to this material on the left wing caused the 2003 Space Shuttle Columbia disaster.[18]
With possible inflatable heat shields, as developed by the US (Low Earth Orbit Flight Test Inflatable Decelerator - LOFTID)[19] and China,[20] single-use rockets like the Space Launch System are considered to be retrofitted with such heat shields to salvage the expensive engines, possibly reducing the costs of launches significantly.[21]
Passive cooling
Passive cooled protectors are used to protect spaceships during atmospheric entry to absorb heat peaks and subsequently irradiate heat to the atmosphere. Early versions included a substantial amount of metals such as titanium, beryllium and copper. This greatly increased the mass of the vehicle. Heat absorption and ablative systems became preferable.
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 X-33. Carbon is the most refractory material known with a sublimation temperature (for graphite) of 3825 °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 Service Module and Lunar Module descent stage.
Military
Heat shields are often affixed to semi-automatic or automatic rifles and shotguns as barrel shrouds in order to protect the user's hands from the heat caused by firing shots in rapid succession. They have also often been affixed to pump-action combat shotguns, allowing the soldier to grasp the barrel while using a bayonet.[citation needed]
Industry
Heat shields are used in metallurgical industry to protect structural steel of the building or other equipment from the high temperature of nearby liquid metal.[citation needed]
^Fahrenholtz, William G; Wuchina, Eric J; Lee, William E; Zhou, Yanchun, eds. (2014). "Ultra-High Temperature Ceramics: Materials for Extreme Environment Applications". doi:10.1002/9781118700853. ISBN9781118700853.
^Leinbach, Micheal D.; Ward, Jonathan H. (2020). Bringing Columbia Home: The Untold True Story of a Lost Space Shuttle and Her Crew. New York, NY: Arcade Publishing. pp. 229–234. ISBN9781948924610.
