Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:New_Zealand
|
| gptkbp:cycle |
electric pump-fed
|
| gptkbp:firstFlight |
2017
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:ispVacuum |
343 s
|
| gptkbp:manufacturer |
gptkb:Rocket_Lab
|
| gptkbp:material |
3D-printed components
|
| gptkbp:namedAfter |
gptkb:Ernest_Rutherford
|
| gptkbp:notableFeature |
first electric-pump-fed engine to power an orbital rocket
|
| gptkbp:numberOfEnginesPerElectronFirstStage |
9
|
| gptkbp:numberOfEnginesPerElectronSecondStage |
1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:status |
in service
|
| gptkbp:thrustSeaLevel |
311 s
24 kN |
| gptkbp:thrustVacuum |
25 kN
|
| gptkbp:usedIn |
gptkb:Electron_rocket
|
| gptkbp:bfsParent |
gptkb:Rocket_Lab
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rutherford engine
|