Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:engineType |
gptkb:F-1
gptkb:J-2 |
| gptkbp:firstFlight |
1967
|
| gptkbp:fuelType |
gptkb:RP-1
liquid hydrogen |
| https://www.w3.org/2000/01/rdf-schema#label |
Saturn V rocket engines
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:numberOnFirstStage |
5 (F-1 engines)
|
| gptkbp:numberOnSecondStage |
5 (J-2 engines)
|
| gptkbp:numberOnThirdStage |
1 (J-2 engine)
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
F-1: 1,522,000 lbf
J-2: 230,000 lbf |
| gptkbp:usedFor |
gptkb:Apollo_program
Skylab launch |
| gptkbp:usedIn |
gptkb:Saturn_V
|
| gptkbp:usedOnStage |
first stage
third stage second stage |
| gptkbp:bfsParent |
gptkb:Santa_Susana_Field_Laboratory
|
| gptkbp:bfsLayer |
6
|