Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:burnTime |
280 seconds
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator cycle
|
| gptkbp:diameter |
1.02 m
|
| gptkbp:firstFlight |
1957
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rocketdyne LR79
|
| gptkbp:length |
3.4 m
|
| gptkbp:manufacturer |
gptkb:Rocketdyne
|
| gptkbp:propulsion |
gptkb:RP-1
liquid oxygen |
| gptkbp:status |
retired
|
| gptkbp:thrustSeaLevel |
607 kN
|
| gptkbp:thrustVacuum |
667 kN
|
| gptkbp:usedIn |
gptkb:Atlas_missile
gptkb:SM-65_Atlas gptkb:Atlas-Agena_launch_vehicle gptkb:Mercury-Atlas_launches gptkb:Atlas-Centaur gptkb:Atlas_D Atlas E/F ICBM |
| gptkbp:weight |
1,090 kg
|
| gptkbp:bfsParent |
gptkb:Thor_missile
|
| gptkbp:bfsLayer |
5
|