Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:culturalHeritage |
gptkb:Falcon_9_second_stage
|
| gptkbp:diameter |
3.66 m
|
| gptkbp:engine |
gptkb:Merlin_Vacuum
|
| gptkbp:fuelType |
gptkb:RP-1
107,500 kg |
| gptkbp:guidanceSystem |
autonomous
|
| https://www.w3.org/2000/01/rdf-schema#label |
Falcon Heavy second stage
|
| gptkbp:length |
12.6 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:material |
aluminum-lithium alloy
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:partOf |
gptkb:Falcon_Heavy
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:reusable |
no
|
| gptkbp:thrustVacuum |
934 kN
|
| gptkbp:used_in |
gptkb:Falcon_Heavy_launches
|
| gptkbp:usedFor |
orbital insertion
payload deployment |
| gptkbp:bfsParent |
gptkb:Merlin_1D_Vacuum
|
| gptkbp:bfsLayer |
7
|