Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designer |
gptkb:SpaceX
|
| gptkbp:engineCycle |
gas-generator cycle
|
| gptkbp:firstFlight |
2010
|
| https://www.w3.org/2000/01/rdf-schema#label |
Merlin 1D Vacuum
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:nozzleExpansionRatio |
165:1
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:specificImpulseVacuum |
348 s
|
| gptkbp:status |
active
|
| gptkbp:throttleable |
yes
|
| gptkbp:thrustVacuum |
981 kN
|
| gptkbp:usedFor |
orbital insertion
payload deployment |
| gptkbp:usedIn |
gptkb:Falcon_9_second_stage
|
| gptkbp:usedOn |
gptkb:Falcon_Heavy_second_stage
|
| gptkbp:bfsParent |
gptkb:Falcon_9_v1.1
|
| gptkbp:bfsLayer |
6
|