Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
rocket engine family
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:Rocketdyne
gptkb:Aerojet |
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
gptkb:Aerozine_50
gptkb:RP-1 |
| https://www.w3.org/2000/01/rdf-schema#label |
Titan rocket engines
|
| gptkbp:notableModel |
gptkb:LR-87
gptkb:LR-91 |
| gptkbp:oxidizer |
liquid oxygen
nitrogen tetroxide |
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
430 kN to 2,400 kN
|
| gptkbp:usedFor |
gptkb:satellite
gptkb:ICBM |
| gptkbp:usedIn |
gptkb:Titan_I
gptkb:Titan_II gptkb:Titan_III gptkb:Titan_IV |
| gptkbp:bfsParent |
gptkb:Aerojet
|
| gptkbp:bfsLayer |
6
|