Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
5.1 m
|
| gptkbp:engine |
gptkb:RL10B-2
|
| gptkbp:firstFlight |
2002
|
| gptkbp:lastFlight |
2024
|
| gptkbp:length |
12.2 m
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
liquid hydrogen
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
110 kN
|
| gptkbp:usedOn |
gptkb:Delta_IV
gptkb:Delta_IV_Heavy gptkb:Delta_IV_Medium |
| gptkbp:bfsParent |
gptkb:AJ10
gptkb:Aerojet_Rocketdyne_AJ10 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Delta IV second stage
|