Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| gptkbp:manufacturer |
gptkb:Aerojet
|
| gptkbp:oxidizer |
nitrogen tetroxide
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:specificImpulseVacuum |
316 seconds
|
| gptkbp:status |
retired
|
| gptkbp:thrustVacuum |
453 kN
|
| gptkbp:usedIn |
gptkb:Titan_23G
gptkb:Titan_I gptkb:Titan_II gptkb:Titan_III gptkb:Gemini-Titan_II |
| gptkbp:bfsParent |
gptkb:Titan_II_SLV_Missile
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
LR91 (second stage)
|