Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:diameter |
2.4 m
|
| gptkbp:engine |
Aerojet AJ10-118K
|
| gptkbp:guidanceSystem |
inertial guidance
|
| gptkbp:length |
6.0 m
|
| gptkbp:manufacturer |
gptkb:Aerojet
|
| gptkbp:propulsion |
gptkb:Aerozine_50
gptkb:dinitrogen_tetroxide |
| gptkbp:thrust |
43.4 kN
|
| gptkbp:usedOn |
gptkb:Delta_6000
gptkb:Delta_7000 gptkb:Delta_2000 gptkb:Delta_3000 gptkb:Delta_5000 gptkb:Delta_II Delta 4000 |
| gptkbp:bfsParent |
gptkb:Aerozine_50/Nitrogen_tetroxide
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Delta II second stage
|