Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:application |
gptkb:Space_Launch_System
|
| gptkbp:designed_by |
gptkb:Aerojet_Rocketdyne
|
| gptkbp:first_flight |
gptkb:2015
|
| gptkbp:fuel_type |
liquid hydrogen
|
| https://www.w3.org/2000/01/rdf-schema#label |
RL10-CE2
|
| gptkbp:oxidation_states |
liquid oxygen
|
| gptkbp:propulsion |
22,300 lbf
|
| gptkbp:specific_impulse |
450 seconds
|
| gptkbp:status |
in service
|
| gptkbp:used_in |
Centaur upper stage
|
| gptkbp:bfsParent |
gptkb:RL10_engine
|
| gptkbp:bfsLayer |
5
|