Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:attachedTo |
Command Module structure
|
| gptkbp:criticalFor |
astronaut safety
|
| gptkbp:developedBy |
gptkb:NASA
|
| gptkbp:diameter |
about 12.8 feet
|
| gptkbp:function |
protect against reentry heat
|
| https://www.w3.org/2000/01/rdf-schema#label |
Command Module Heat Shield
|
| gptkbp:inspectedAfterFlight |
yes
|
| gptkbp:introducedIn |
gptkb:Apollo_1_(AS-204)
|
| gptkbp:location |
base of Command Module
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
|
| gptkbp:material |
gptkb:Avcoat
ablative material |
| gptkbp:mission |
gptkb:Apollo_11
gptkb:Apollo_13 gptkb:Apollo_17 |
| gptkbp:removedAfterMission |
yes
|
| gptkbp:replacedBy |
Orion heat shield
|
| gptkbp:shape |
blunt cone
|
| gptkbp:technology |
ablative heat shield
|
| gptkbp:testedBy |
gptkb:White_Sands_Test_Facility
|
| gptkbp:usedOn |
gptkb:satellite
|
| gptkbp:weight |
about 3,000 pounds
|
| gptkbp:withstandsTemperature |
up to 5,000 degrees Fahrenheit
|
| gptkbp:bfsParent |
gptkb:Apollo_hardware
|
| gptkbp:bfsLayer |
7
|