Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.3 m
|
| gptkbp:engineCycle |
pressure-fed
|
| gptkbp:engineType |
hypergolic
|
| gptkbp:firstFlight |
2015
|
| gptkbp:gimbalRange |
15 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
SuperDraco thruster
|
| gptkbp:length |
0.81 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:numberOfEnginesPerCrewDragon |
8
|
| gptkbp:propulsion |
monomethylhydrazine
nitrogen tetroxide |
| gptkbp:relatedTo |
gptkb:Draco_thruster
|
| gptkbp:reusable |
yes
|
| gptkbp:seaLevelSpecificImpulse |
210 s
|
| gptkbp:status |
active
|
| gptkbp:thrust |
73 kN
|
| gptkbp:usedFor |
launch escape system
orbital maneuvering |
| gptkbp:usedIn |
gptkb:Crew_Dragon
|
| gptkbp:vacuumSpecificImpulse |
235 s
|
| gptkbp:bfsParent |
gptkb:SpaceX
|
| gptkbp:bfsLayer |
5
|