Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Ablative heat shield material
|
| gptkbp:application |
filled into honeycomb cells and cured in place
|
| gptkbp:color |
orange-brown
|
| gptkbp:composition |
epoxy novolac resin with silica fibers in a honeycomb matrix
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:density |
~32 lb/ft³ (512 kg/m³)
|
| gptkbp:developedBy |
gptkb:Avco_Corporation
|
| gptkbp:function |
protect spacecraft from reentry heat
|
| https://www.w3.org/2000/01/rdf-schema#label |
Avcoat
|
| gptkbp:introducedIn |
1960s
|
| gptkbp:manufacturer |
gptkb:Hexcel_Corporation
|
| gptkbp:NASAStandard |
gptkb:NASA-STD-6016
|
| gptkbp:notableMission |
gptkb:Apollo_11
gptkb:Artemis_I |
| gptkbp:purpose |
thermal protection
|
| gptkbp:relatedTo |
Ablative material
|
| gptkbp:replacedBy |
PICA (Phenolic Impregnated Carbon Ablator) in some missions
|
| gptkbp:restored |
gptkb:Orion_MPCV
|
| gptkbp:status |
in use as of 2022
|
| gptkbp:usedIn |
gptkb:satellite
gptkb:Orion_Crew_Module |
| gptkbp:bfsParent |
gptkb:Orion_spacecraft
|
| gptkbp:bfsLayer |
5
|