Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:chamberPressure |
4.8 MPa
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:Rocketdyne
late 1950s |
| gptkbp:diameter |
2.1 m
|
| gptkbp:engineCycle |
gas-generator
|
| gptkbp:firstTestMatch |
1959
|
| gptkbp:fuelType |
gptkb:RP-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
E-1 rocket engine
|
| gptkbp:intendedUse |
gptkb:Saturn_I_rocket
first stage booster |
| gptkbp:length |
4.2 m
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:replacedBy |
gptkb:F-1_rocket_engine
|
| gptkbp:status |
cancelled
|
| gptkbp:thrustSeaLevel |
1,000 kN
|
| gptkbp:thrustVacuum |
1,500 kN
|
| gptkbp:usedIn |
never flown
|
| gptkbp:weight |
2,200 kg
|
| gptkbp:bfsParent |
gptkb:Rocketdyne
|
| gptkbp:bfsLayer |
6
|