Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
5.1 m
|
| gptkbp:engine |
gptkb:RS-68A
|
| gptkbp:firstFlight |
2002
|
| gptkbp:fuelTankMaterial |
aluminum-lithium alloy
|
| gptkbp:guidanceSystem |
inertial guidance
|
| gptkbp:launchSite |
gptkb:Cape_Canaveral_Space_Launch_Complex_37B
gptkb:Vandenberg_Space_Launch_Complex_6 |
| gptkbp:length |
40.8 m
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:retired |
2024
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
3,137 kN
|
| gptkbp:usedAsFirstStage |
gptkb:Delta_IV_Medium
|
| gptkbp:usedAsStrapOnBooster |
gptkb:Delta_IV_Heavy
|
| gptkbp:usedIn |
gptkb:Delta_IV
gptkb:Delta_IV_Heavy |
| gptkbp:bfsParent |
gptkb:Delta_IV_Heavy
gptkb:Boeing_Delta_IV_Heavy |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Common Booster Core
|