Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.3 m
|
| gptkbp:engineCycle |
pressure-fed
|
| gptkbp:engineType |
hypergolic
|
| gptkbp:fabricationProcess |
3D printing
|
| gptkbp:firstFlight |
2012
|
| gptkbp:gimbalRange |
15 degrees
|
| gptkbp:ISPseaLevel |
210 s
|
| gptkbp:ISPvac |
235 s
|
| gptkbp:length |
0.81 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:material |
gptkb:Inconel
|
| gptkbp:numberOfEnginesPerCrewDragon |
8
|
| gptkbp:oxidizer |
nitrogen tetroxide
|
| gptkbp:propulsion |
monomethylhydrazine
|
| gptkbp:reusable |
true
|
| gptkbp:status |
active
|
| gptkbp:throttleable |
true
|
| gptkbp:thrust |
73 kN
|
| gptkbp:usedFor |
gptkb:launch_escape_system
orbital maneuvering |
| gptkbp:usedIn |
gptkb:In-Flight_Abort_Test_(2020)
gptkb:Pad_Abort_Test_(2015) gptkb:Crew_Dragon gptkb:Dragon_2 |
| gptkbp:bfsParent |
gptkb:Tom_Mueller
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
SuperDraco rocket engine
|