Space Shuttle thermal protection system

E175049

The Space Shuttle thermal protection system was a complex arrangement of heat-resistant tiles, blankets, and reinforced carbon-carbon designed to shield the orbiter from the extreme temperatures of atmospheric reentry.

All labels observed (6)

How this entity was disambiguated

Statements (49)

Predicate Object
instanceOf aerospace engineering subsystem ⓘ
spacecraft thermal protection system ⓘ
appliedTo orbiter nose cap ⓘ
orbiter payload bay doors ⓘ
orbiter underside ⓘ
orbiter upper surfaces ⓘ
orbiter vertical tail ⓘ
orbiter wing leading edges ⓘ
certifiedBy NASA Johnson Space Center ⓘ
countryOfOrigin United States ⓘ
designedFor protection from aerodynamic heating ⓘ
thermal protection during atmospheric reentry ⓘ
developedBy NASA ⓘ
developedForProgram Space Shuttle program ⓘ
failureContributedTo Space Shuttle Columbia disaster ⓘ
linked to: Columbia disaster
includesComponent Advanced Flexible Reusable Surface Insulation ⓘ
FIB blankets ⓘ
FRCI-12 tiles ⓘ
HRSI tiles ⓘ
LI-2200 silica tiles ⓘ
LI-900 silica tiles ⓘ
LRSI tiles ⓘ
gap fillers ⓘ
reinforced carbon–carbon ⓘ
thermal barrier seals ⓘ
locatedOn orbiter external surface ⓘ
mass approximately 9,575 kilograms ⓘ
materialType carbon–carbon composite ⓘ
low-density silica ceramic ⓘ
quartz fabric insulation blanket ⓘ
maxDesignTemperature approximately 1650 °C ⓘ
operationalFrom 1981 ⓘ
operationalUntil 2011 ⓘ
partOf Space Shuttle orbiter ⓘ
primaryFunction limit orbiter structural temperature to safe levels ⓘ
protectsStructure aluminum airframe of orbiter ⓘ
requires extensive inspection between flights ⓘ
tile repair and replacement between missions ⓘ
reusable true ⓘ
supportsOperationPhase ascent ⓘ
reentry ⓘ
testedAt NASA Ames Research Center arc-jet facilities ⓘ
tileCount approximately 24,000 tiles ⓘ
usedOn NASA Space Shuttle ⓘ
linked to: Space Shuttle
usesDesignPrinciple ablative and insulative thermal protection ⓘ
emissive cooling ⓘ
low thermal conductivity ⓘ
vulnerableTo foam shedding from external tank ⓘ
impact damage ⓘ

How these facts were elicited

Referenced by (7)

Full triples — surface form annotated when it differs from this entity's canonical label.

STS-1 → tested → Space Shuttle thermal protection system ⓘ
Space Shuttle thermal protection system → includesComponent → Advanced Flexible Reusable Surface Insulation ⓘ
linked to: Space Shuttle thermal protection system
NASA PICA → belongsToProgram → NASA thermal protection system development program ⓘ
linked to: Space Shuttle thermal protection system
LI-2200 silica tiles → partOf → Space Shuttle Thermal Protection System ⓘ
linked to: Space Shuttle thermal protection system
LI-900 silica tiles → appliedTo → Space Shuttle lower surface ⓘ
linked to: Space Shuttle thermal protection system
LI-900 silica tiles → appliedTo → Space Shuttle leading edges vicinity ⓘ
linked to: Space Shuttle thermal protection system
STS-3 → testedSystem → Space Shuttle thermal protection system ⓘ
subject linked to: Jack R. Lousma – STS-3