Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:diameter |
1.7 m
|
| gptkbp:engineType |
gptkb:Merlin_1A
gptkb:Merlin_1C |
| gptkbp:length |
21.3 ft
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:material |
aluminum-lithium alloy
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:reusable |
no
|
| gptkbp:thrustSeaLevel |
318 kN
|
| gptkbp:usedInFlights |
gptkb:Falcon_1_Flight_1
gptkb:Falcon_1_Flight_3 gptkb:Falcon_1_Flight_4 gptkb:Falcon_1_Flight_5 gptkb:Falcon_1_Flight_2 |
| gptkbp:usedOn |
gptkb:Falcon_1
|
| gptkbp:bfsParent |
gptkb:Merlin_engine
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Falcon 1 first stage
|