Triple
T1523623
| Position | Surface form | Disambiguated ID | Type / Status |
|---|---|---|---|
| Subject | Rockwell International |
E32284
|
entity |
| Predicate | developed |
P73
|
FINISHED |
| Object |
Saturn V S-II second stage
The Saturn V S-II second stage was the liquid hydrogen–fueled second stage of NASA’s Saturn V Moon rocket, providing the crucial mid-ascent propulsion that enabled Apollo missions to reach Earth orbit and proceed toward the Moon.
|
E179083
|
NE FINISHED |
Provenance (5 batches)
| Stage | Batch ID | Job type | Status |
|---|---|---|---|
| creating | batch_69a885e9b0ac819093a9806ad0efc82c |
elicitation | completed |
| NER | batch_69a90800433c8190b23ae2860493a16e |
ner | completed |
| NED1 | batch_69ad401616ec81908edd9dcb9f4a0184 |
ned_source_triple | completed |
| NED2 | batch_69ad41968e4c8190b843b97e18ac9968 |
ned_description | completed |
| NEDg | batch_69ad4130bf30819092be42a4e9225220 |
nedg | completed |
Created at: March 4, 2026, 7:26 p.m.