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 (3)

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 Johnson Space Center
surface form: NASA Johnson Space Center
countryOfOrigin United States of America
surface form: United States
designedFor protection from aerodynamic heating
thermal protection during atmospheric reentry
developedBy NASA
developedForProgram NASA Space Shuttle program
surface form: Space Shuttle program
failureContributedTo Columbia disaster
surface form: Space Shuttle Columbia disaster
includesComponent Space Shuttle thermal protection system self-linksurface differs
surface form: 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 Space Shuttle
surface form: NASA 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 (3)

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 Space Shuttle thermal protection system self-linksurface differs
this entity surface form: Advanced Flexible Reusable Surface Insulation
NASA PICA belongsToProgram Space Shuttle thermal protection system
this entity surface form: NASA thermal protection system development program