Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.3 m
|
| gptkbp:engineCycle |
pressure-fed
|
| gptkbp:engineType |
liquid rocket engine
|
| gptkbp:firstFlight |
2015
|
| gptkbp:fuelType |
monomethylhydrazine
|
| gptkbp:gimbalRange |
15 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
SuperDraco abort engines
|
| gptkbp:length |
0.81 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:numberOfEnginesPerCapsule |
8
|
| gptkbp:oxidizer |
nitrogen tetroxide
|
| gptkbp:primaryUse |
launch escape system
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:reusable |
true
|
| gptkbp:status |
active
|
| gptkbp:thrust |
73 kN
|
| gptkbp:usedFor |
in-flight abort test
pad abort test |
| gptkbp:usedIn |
gptkb:Crew_Dragon
|
| gptkbp:usedOn |
gptkb:Crew_Dragon_Demo-1
gptkb:Crew_Dragon_In-Flight_Abort_Test |
| gptkbp:weight |
45 kg
|
| gptkbp:bfsParent |
gptkb:Cargo_Dragon_spacecraft
|
| gptkbp:bfsLayer |
7
|