Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.66 meters
|
| gptkbp:engine |
gptkb:Merlin_Vacuum
|
| gptkbp:firstFlight |
2010
|
| gptkbp:fuelType |
107,500 kg
|
| gptkbp:guidanceSystem |
autonomous
|
| https://www.w3.org/2000/01/rdf-schema#label |
Falcon 9 upper stage
|
| gptkbp:length |
12.6 meters
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:partOf |
gptkb:Falcon_9
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:reusable |
no
|
| gptkbp:status |
active
|
| gptkbp:thrustVacuum |
981 kN
|
| gptkbp:used_in |
gptkb:Falcon_9_v1.0
gptkb:Falcon_9_Full_Thrust gptkb:Falcon_9_Block_5 gptkb:Falcon_9_v1.1 |
| gptkbp:usedFor |
orbital insertion
payload deployment |
| gptkbp:bfsParent |
gptkb:Starship_second_stage
|
| gptkbp:bfsLayer |
8
|