Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
5.4 meters
|
| gptkbp:engineType |
gptkb:RL10
|
| gptkbp:firstFlight |
2024
|
| gptkbp:fuelType |
over 60,000 kg
|
| https://www.w3.org/2000/01/rdf-schema#label |
Vulcan Centaur upper stage
|
| gptkbp:length |
12.7 meters
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:missionType |
orbital insertion
payload deployment |
| gptkbp:numberOfEngines |
2
|
| gptkbp:partOf |
gptkb:Vulcan_launch_vehicle
|
| gptkbp:predecessor |
gptkb:Centaur_upper_stage
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
in development
|
| gptkbp:usedOn |
gptkb:Vulcan_rocket
|
| gptkbp:bfsParent |
gptkb:RL10_engine
|
| gptkbp:bfsLayer |
6
|