NASA PICA

E277912

NASA PICA is a lightweight, ablative heat shield material developed by NASA for protecting spacecraft during high-speed atmospheric entry.

All labels observed (1)

Label Occurrences
NASA PICA canonical 1

How this entity was disambiguated

Statements (47)

Predicate Object
instanceOf ablative heat shield material
thermal protection system material
abbreviationFor Phenolic-Impregnated Carbon Ablator
applicationPhase entry, descent, and landing (EDL)
belongsToProgram Space Shuttle thermal protection system
surface form: NASA thermal protection system development program
category reentry vehicle materials
spacecraft heat shield technology
componentMaterial carbon fiber preform
phenolic resin
density approximately 0.27 g/cm³
developedFor Earth atmospheric entry
Mars atmospheric entry
high-velocity sample return missions
developer NASA
Ames Research Center
surface form: NASA Ames Research Center
hasProperty ablative
high heat-flux capability
high recession resistance
lightweight
low density
low thermal conductivity
low thermal diffusivity
heatShieldForm monolithic forebody heat shield tiles
improvedUpon earlier carbon phenolic ablators for some mission profiles
manufacturingProcess curing and machining into heat shield tiles
impregnation of carbon preform with phenolic resin
materialClass phenolic-impregnated carbon ablator
notableMission Mars Science Laboratory
surface form: Mars Science Laboratory Curiosity (2012 Mars entry)

NASA Stardust mission
surface form: Stardust comet sample return (2006 Earth reentry)
operatingEnvironment high-enthalpy flow
hypersonic atmospheric entry
performanceRange suitable for very high heat flux and pressure environments
relatedMaterial PICA-X
relatedOrganization Johnson Space Center
surface form: NASA Johnson Space Center

Langley Research Center
surface form: NASA Langley Research Center
structureType rigid, low-density carbon fiber matrix
testedAt NASA Ames Research Center arc-jet facilities
surface form: NASA Ames arc-jet facilities
thermalProtectionMechanism ablation
char layer formation
pyrolysis gas release
usedFor high-speed atmospheric entry
protection of spacecraft heat shields
sample return missions
thermal protection during atmospheric entry
usedOnSpacecraft Mars Science Laboratory Curiosity rover heat shield
Crew Dragon
surface form: SpaceX Dragon capsule (PICA-X variant)

Stardust mission
surface form: Stardust sample return capsule

How these facts were elicited

Referenced by (1)

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

PICA-X basedOn NASA PICA