Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
8.4 meters
|
| gptkbp:engine |
gptkb:RS-25
|
| gptkbp:firstFlight |
2022
|
| gptkbp:height |
65 meters
|
| gptkbp:launchSite |
gptkb:Kennedy_Space_Center
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:mass_(empty) |
85,000 kg
|
| gptkbp:mass_(fully_fueled) |
972,000 kg
|
| gptkbp:material |
aluminum-lithium alloy
|
| gptkbp:numberOfEngines |
4
|
| gptkbp:partOf |
gptkb:Space_Launch_System
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
active
|
| gptkbp:successor |
gptkb:Space_Shuttle_External_Tank
|
| gptkbp:thrustSeaLevel |
8,870 kN
|
| gptkbp:used_on_mission |
gptkb:Artemis_I
|
| gptkbp:usedFor |
deep space missions
|
| gptkbp:bfsParent |
gptkb:RS-25_engine
gptkb:RS-25_rocket_engine gptkb:RS-25 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
SLS core stage
|