Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:boosters |
2
|
| gptkbp:coreCount |
3
|
| gptkbp:coreReuse |
possible
|
| gptkbp:diameter |
3.66 m
|
| gptkbp:engineType |
gptkb:Merlin_1D
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:guidanceSystem |
autonomous
|
| https://www.w3.org/2000/01/rdf-schema#label |
Falcon Heavy first stage
|
| gptkbp:landingCapability |
vertical landing
|
| gptkbp:length |
42.6 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:material |
aluminum-lithium alloy
|
| gptkbp:numberOfEnginesPerCore |
9
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:partOf |
gptkb:Falcon_Heavy
|
| gptkbp:reusable |
true
|
| gptkbp:sideBoosterReuse |
possible
|
| gptkbp:thrustSeaLevel |
22,819 kN
|
| gptkbp:totalNumberOfEngines |
27
|
| gptkbp:usedOnFirstFlight |
6 February 2018
|
| gptkbp:bfsParent |
gptkb:Merlin_engine
|
| gptkbp:bfsLayer |
6
|