Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine
|
| gptkbp:application |
launch vehicles
|
| gptkbp:barrelLength |
1,200 psi
|
| gptkbp:chemicalFormula |
liquid oxygen
|
| gptkbp:coolingSystem |
regenerative cooling
|
| gptkbp:developer |
NASA
|
| gptkbp:diameter |
5 ft
|
| gptkbp:engine |
8
|
| gptkbp:engineType |
liquid-fueled
|
| gptkbp:firstFlight |
1961
1975 |
| gptkbp:fuelType |
RP-1
gas-generator cycle |
| gptkbp:hasDepartment |
150 seconds
|
| https://www.w3.org/2000/01/rdf-schema#label |
RB 41
|
| gptkbp:is_used_in |
Saturn I
|
| gptkbp:length |
12 ft
|
| gptkbp:manufacturer |
Rocketdyne
|
| gptkbp:operational_status |
retired
|
| gptkbp:propulsion |
300 seconds
150,000 lbf |
| gptkbp:successor |
J-2 engine
|
| gptkbp:weight |
1,500 lb
|