Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
5.4 m
|
| gptkbp:engineType |
gptkb:BE-4
|
| gptkbp:firstFlight |
2024
|
| https://www.w3.org/2000/01/rdf-schema#label |
Vulcan Centaur first stage
|
| gptkbp:length |
40.8 m
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:partOf |
gptkb:Vulcan_Centaur
|
| gptkbp:propulsion |
liquefied natural gas
liquid oxygen |
| gptkbp:reusable |
no
|
| gptkbp:thrust |
2,400 kN (per engine)
|
| gptkbp:usedOn |
gptkb:Vulcan_launch_vehicle
|
| gptkbp:bfsParent |
gptkb:BE-4
|
| gptkbp:bfsLayer |
6
|