Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket upper stage
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
5.4 meters
|
| gptkbp:engineType |
gptkb:RL10C
RL10C-1-1 |
| gptkbp:firstFlight |
planned 2024
|
| https://www.w3.org/2000/01/rdf-schema#label |
Centaur V
|
| gptkbp:length |
12.2 meters
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:numberOfEngines |
2
4 |
| gptkbp:predecessor |
gptkb:Centaur_III
|
| gptkbp:primaryMission |
upper stage for heavy-lift launch vehicles
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
in development
|
| gptkbp:thrust |
2 x 110 kN
|
| gptkbp:usedFor |
payload insertion to GTO and beyond
|
| gptkbp:usedOn |
gptkb:Atlas_V_N22
gptkb:Vulcan_Centaur Vulcan VC4 Vulcan VC6 |
| gptkbp:bfsParent |
gptkb:Vulcan_Centaur_rocket
gptkb:RL10 |
| gptkbp:bfsLayer |
6
|