Triple

T12738645
Position Surface form Disambiguated ID Type / Status
Subject Mobile Launcher 2 E304429 entity
Predicate compatibleWith P203 FINISHED
Object Saturn V third stage (S-IVB) E130633 NE FINISHED

How this triple was built (2 steps)

Every LLM step that produced this triple, in pipeline order — named-entity classification, the disambiguation choices (the exact options shown, with the pick highlighted), and the generated description. The batch + timestamp of each is in the Provenance table below.

NER Named-entity recognition gpt-5-mini
Instruction
Given a phrase, classify it is english named entity (e.g., persons, organizations, works of art) in Latin script, or not (e.g., literals, dates, URLs, verbose phrases). For disambiguation, the statement where the phrase occurs as object is also given. Please return a JSON object with `phrase` (string, the phrase being analyzed) and `is_ne` (boolean, indicating whether the phrase is a Named Entity).
Input
Phrase: Saturn V third stage (S-IVB) | Statement: [Mobile Launcher 2, compatibleWith, Saturn V third stage (S-IVB)]
NED1 Entity disambiguation (via context triple) gpt-5-mini-2025-08-07
Target entity: Saturn V third stage (S-IVB)
Context triple: [Mobile Launcher 2, compatibleWith, Saturn V third stage (S-IVB)]
  • A. S-IVB chosen
    The S-IVB was the single-engine upper stage of NASA’s Saturn launch vehicles, used to place Apollo spacecraft into Earth orbit and send them toward the Moon.
  • B. 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.
  • C. Saturn V first stage (S-IC)
    The Saturn V first stage (S-IC) was the massive, kerosene-fueled lower stage of NASA’s Saturn V rocket, providing the initial thrust to lift Apollo missions off the launch pad and through the lower atmosphere.
  • D. S-IV
    S-IV was the liquid-fueled second stage of the early Saturn I launch vehicle, powered by a cluster of RL10 engines and used in NASA’s Apollo-era test flights.
  • E. Saturn V instrument unit
    The Saturn V instrument unit was the ring-shaped electronic control and guidance section that housed the rocket’s navigation, telemetry, and flight control systems.
  • F. None of above.
  • G. Unsure - the case is ambiguous/there is not enough information to decide.

Provenance (3 batches)

The batch behind each pipeline step, in order, with when it ran. Timestamps are batch-level — stages were processed in waves, so the object chain (NER → NED1 → NEDg → NED2) reads in order, but predicate / elicitation batches can sit in a different wave.

Step Stage Batch ID Status When
creating Elicitation batch_69d7bdf1426c8190a4402e1c4cdec33a completed April 9, 2026, 2:55 p.m.
NER Named-entity recognition batch_69d9646cfcac81909283dca987755c0e completed April 10, 2026, 8:58 p.m.
NED1 Entity disambiguation (via context triple) batch_69f68eb388488190a30866e9a7a0bc41 completed May 2, 2026, 11:54 p.m.
Created at: April 9, 2026, 5:26 p.m.