Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:rocket_engine_family
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:North_American_Aviation
|
| gptkbp:engineType |
liquid-propellant rocket engine
|
| gptkbp:firstFlight |
1957
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:thrust |
about 667 kN
|
| gptkbp:usedIn |
gptkb:Thor-Able
gptkb:satellite gptkb:Thor-Agena gptkb:Thor_missile gptkb:PGM-17_Thor early Delta launch vehicles |
| gptkbp:bfsParent |
gptkb:Santa_Susana_Field_Laboratory
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Thor rocket engines
|