Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChamberMaterial |
ablative cooled carbon fiber
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
pressure-fed
|
| gptkbp:engineType |
liquid rocket engine
|
| gptkbp:firstFlight |
2006
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:gimbalRange |
±5 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kestrel rocket engine
|
| gptkbp:lastFlight |
2009
|
| gptkbp:manufacturer |
gptkb:SpaceX
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
282 s
317 s |
| gptkbp:status |
retired
|
| gptkbp:thrustSeaLevel |
25.7 kN
|
| gptkbp:thrustVacuum |
31 kN
|
| gptkbp:usedAs |
second stage engine
|
| gptkbp:usedBy |
gptkb:SpaceX
|
| gptkbp:usedIn |
gptkb:Falcon_1
|
| gptkbp:bfsParent |
gptkb:SpaceX
|
| gptkbp:bfsLayer |
5
|