Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:assemblyLocation |
gptkb:Michoud_Assembly_Facility
|
| gptkbp:contains |
intertank
liquid hydrogen tank liquid oxygen tank engine section forward skirt |
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
8.4 meters
|
| gptkbp:engineType |
gptkb:RS-25
|
| gptkbp:firstFlight |
2022
|
| gptkbp:height |
65 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
NASA SLS core stage
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:massWhenFueled |
about 2,300,000 kg
|
| gptkbp:numberOfEngines |
4
|
| gptkbp:partOf |
gptkb:Space_Launch_System
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:thrust |
about 8.8 million pounds
|
| gptkbp:usedIn |
gptkb:Artemis_I
|
| gptkbp:bfsParent |
gptkb:RS-25E
|
| gptkbp:bfsLayer |
7
|