Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
0.19 m
|
| gptkbp:engineCycle |
pressure-fed
|
| gptkbp:engineMaterial |
gptkb:Inconel
|
| gptkbp:firstFlight |
2010
|
| https://www.w3.org/2000/01/rdf-schema#label |
Draco rocket engine
|
| gptkbp:length |
0.28 m
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:numberOfEnginesOnDragon |
16
|
| gptkbp:oxidizer |
nitrogen tetroxide
|
| gptkbp:propulsion |
monomethylhydrazine
|
| gptkbp:restartable |
yes
|
| gptkbp:seaLevelSpecificImpulse |
260 s
|
| gptkbp:status |
active
|
| gptkbp:successor |
gptkb:SuperDraco_rocket_engine
|
| gptkbp:thrust |
400 N
|
| gptkbp:type |
hypergolic
|
| gptkbp:usedFor |
attitude control
orbital maneuvering reaction control system |
| gptkbp:usedIn |
gptkb:Cargo_Dragon
gptkb:Crew_Dragon gptkb:Dragon_2_spacecraft SpaceX Dragon spacecraft |
| gptkbp:vacuumSpecificImpulse |
300 s
|
| gptkbp:weight |
3.73 kg
|
| gptkbp:bfsParent |
gptkb:Tom_Mueller
|
| gptkbp:bfsLayer |
6
|