Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
2.7 m
|
| gptkbp:engineCycle |
gas-generator
|
| gptkbp:firstFlight |
2010
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Merlin Vacuum (MVac)
|
| gptkbp:length |
3.1 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:nozzleExpansionRatio |
165:1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:specificImpulseVacuum |
348 s
|
| gptkbp:status |
active
|
| gptkbp:thrustSeaLevel |
822 kN
|
| gptkbp:thrustVacuum |
981 kN
|
| gptkbp:usedBy |
gptkb:SpaceX
|
| gptkbp:usedIn |
gptkb:Falcon_9
gptkb:Falcon_Heavy |
| gptkbp:usedOnStage |
second stage
|
| gptkbp:bfsParent |
gptkb:SpaceX_Merlin
gptkb:Merlin_engine |
| gptkbp:bfsLayer |
6
|