Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:abbreviation |
gptkb:EUS
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designedFor |
deep space missions
|
| gptkbp:diameter |
8.4 meters
|
| gptkbp:engineType |
gptkb:RL10C-3
|
| gptkbp:firstFlight |
gptkb:Artemis_IV
|
| https://www.w3.org/2000/01/rdf-schema#label |
Exploration Upper Stage
|
| gptkbp:intendedUse |
SLS Block 1B
|
| gptkbp:length |
21.7 meters
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:numberOfEngines |
4
|
| gptkbp:partOf |
gptkb:NASA_Artemis_program
|
| gptkbp:payloadToTLI |
up to 38 metric tons
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:replacedBy |
gptkb:Interim_Cryogenic_Propulsion_Stage
|
| gptkbp:status |
in development
|
| gptkbp:usedOn |
gptkb:Space_Launch_System
|
| gptkbp:bfsParent |
gptkb:Space_Launch_System_Block_1B
gptkb:SLS_program gptkb:Space_Launch_System_(SLS)_Interim_Cryogenic_Propulsion_Stage gptkb:Space_Launch_System_upper_stage |
| gptkbp:bfsLayer |
7
|