Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine
|
| gptkbp:barrelLength |
1.5 MPa
|
| gptkbp:chemicalFormula |
Liquid Oxygen
|
| gptkbp:communityPartnerships |
various aerospace companies
|
| gptkbp:controls |
digital control
|
| gptkbp:coolingSystem |
regenerative cooling
|
| gptkbp:designedBy |
gptkb:Rocket_Lab
|
| gptkbp:developer |
$5 million
|
| gptkbp:energyEfficiency |
high
|
| gptkbp:engine |
2.5 m
variable various industry awards publicly available potential upgrades active research small satellite launches 3D printed components regenerative cooling significant in small launch market |
| gptkbp:engineConfiguration |
single engine
|
| gptkbp:engineDisplacement |
available online
ongoing 1.1 m |
| gptkbp:engineType |
high
minimal reliable spark plug liquid rocket engine growing community of users |
| gptkbp:firstFlight |
2017
|
| gptkbp:firstMatch |
2016
|
| gptkbp:fuelType |
RP-1
Gas-generator cycle 0.25 kg/s electric pump |
| gptkbp:hasArea |
extensive
Rocket_Lab's_test_site |
| gptkbp:hasContent |
305 seconds
|
| gptkbp:hasDepartment |
about 150 seconds
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rutherford engine
|
| gptkbp:launched |
gptkb:Rocket_Lab
|
| gptkbp:launchSite |
gptkb:Mahia_Peninsula
|
| gptkbp:numberOfEpisodes |
1
|
| gptkbp:operationalStatus |
active
|
| gptkbp:productionCompany |
3D printing
|
| gptkbp:propulsion |
400:1
24 kN |
| gptkbp:related_engine |
staged combustion
|
| gptkbp:usedIn |
gptkb:Electron_rocket
|
| gptkbp:weight |
about 60 kg
|