Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine family
|
| gptkbp:application |
reusable launch vehicles
|
| gptkbp:combustionChambers |
~300 bar
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:engineCycle |
full-flow staged combustion
|
| gptkbp:firstFlight |
2016
|
| gptkbp:fuelType |
liquid methane
|
| https://www.w3.org/2000/01/rdf-schema#label |
Raptor engine family
|
| gptkbp:ispVacuum |
~380 s
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:notableFeature |
full-flow staged combustion cycle
methalox propellant reusability high chamber pressure |
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
liquid methane
liquid oxygen |
| gptkbp:status |
in production
|
| gptkbp:successor |
gptkb:Merlin_engine_family
|
| gptkbp:testLocation |
gptkb:McGregor,_Texas
|
| gptkbp:thrustSeaLevel |
~330 s
~1.85 MN |
| gptkbp:thrustVacuum |
~2 MN
|
| gptkbp:usedBy |
gptkb:SpaceX
|
| gptkbp:usedIn |
gptkb:satellite
gptkb:Super_Heavy |
| gptkbp:variant |
gptkb:Raptor_1
gptkb:Raptor_2 gptkb:Raptor_Vacuum |
| gptkbp:bfsParent |
gptkb:Raptor_Vacuum
|
| gptkbp:bfsLayer |
7
|