Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket upper stage
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
5.4 meters
|
| gptkbp:engineType |
gptkb:RL10C
|
| gptkbp:firstFlight |
2024 (planned)
|
| https://www.w3.org/2000/01/rdf-schema#label |
Centaur V upper stage
|
| gptkbp:length |
12.2 meters
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:missionType |
orbital insertion
payload deployment |
| gptkbp:numberOfEngines |
2
4 |
| gptkbp:predecessor |
gptkb:Centaur_III
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
in development
|
| gptkbp:thrust |
220 kN (per engine)
|
| gptkbp:usedOn |
gptkb:Vulcan_Centaur
|
| gptkbp:bfsParent |
gptkb:RL10_engine
|
| gptkbp:bfsLayer |
6
|