Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:diameter |
2.7 m
|
| gptkbp:firstFlight |
2010
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:gimbalRange |
±8 degrees
|
| gptkbp:hasModel |
gptkb:Merlin
|
| https://www.w3.org/2000/01/rdf-schema#label |
Merlin Vacuum
|
| gptkbp:length |
3.7 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:mass |
approx. 470 kg
|
| gptkbp:nozzleExpansionRatio |
165:1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:predecessor |
gptkb:Merlin_1C_Vacuum
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
348 s
|
| gptkbp:status |
active
|
| gptkbp:successor |
none
|
| gptkbp:thrustVacuum |
981 kN
|
| gptkbp:usedFor |
second stage
|
| gptkbp:usedIn |
gptkb:Falcon_9
gptkb:Falcon_Heavy |
| gptkbp:bfsParent |
gptkb:Falcon_9
gptkb:Falcon_9_launch_vehicle gptkb:Merlin_1D |
| gptkbp:bfsLayer |
5
|