Triple

T1116660

Position	Surface form	Disambiguated ID	Type / Status
Subject	Saturn V	`E11115`	entity
Predicate	secondStage	`P25127`	FINISHED
Object	S-II S-II was the liquid hydrogen–fueled second stage of NASA’s Saturn V rocket, providing the high-thrust propulsion needed to continue Apollo missions toward orbit after first-stage separation.	`E11115`	NE FINISHED

Provenance (7 batches)

Stage	Batch ID	Job type	Status
creating	`batch_69a493252a648190ac48f8742474a5e8`	elicitation	completed
NER	`batch_69a4bc4bc21881909dcfe628f59f3e8c`	ner	completed
NED1	`batch_69ac53999b3c8190aff1cf84a3c16909`	ned_source_triple	completed
NED2	`batch_69ac55afd8c88190b0f2bbafc33ad8b7`	ned_description	completed
NEDg	`batch_69ac554aec048190821801070d1a4852`	nedg	completed
PD	`batch_69a4bb4562f48190831e959f5f309956`	pd	completed
PDg	`batch_69a4bc47fce48190825d3a877251f789`	pdg	completed

Created at: March 1, 2026, 7:43 p.m.