Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine
|
| gptkbp:application |
launch vehicle
|
| gptkbp:barrelLength |
1,200 psi
|
| gptkbp:chemicalFormula |
liquid oxygen
|
| gptkbp:developer |
1950s
|
| gptkbp:firstFlight |
1961
1975 |
| gptkbp:fuelType |
RP-1
|
| gptkbp:hasDepartment |
150 seconds
|
| https://www.w3.org/2000/01/rdf-schema#label |
RB 68
|
| gptkbp:is_used_in |
Saturn I
|
| gptkbp:manufacturer |
Rocketdyne
|
| gptkbp:produces |
20
|
| gptkbp:propulsion |
150,000 lbf
263 seconds |
| gptkbp:successor |
J-2 engine
|
| gptkbp:weight |
1,500 lb
|