Triple

T5817674
Position Surface form Disambiguated ID Type / Status
Subject S-IC E129026 entity
Predicate guidanceSystemLocation P15256 FINISHED
Object 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.
E551351 NE FINISHED

How this triple was built (5 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 instrument unit | Statement: [S-IC, guidanceSystemLocation, Saturn V instrument unit]
NED1 Entity disambiguation (via context triple) gpt-5-mini-2025-08-07
Target entity: Saturn V instrument unit
Context triple: [S-IC, guidanceSystemLocation, Saturn V instrument unit]
  • A. S-IVB
    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 IB
    Saturn IB was a two-stage American launch vehicle used by NASA in the 1960s and early 1970s to test Apollo spacecraft in Earth orbit and support missions such as Apollo–Soyuz.
  • D. Mercury Transfer Module
    The Mercury Transfer Module is the propulsion and support unit of the BepiColombo mission that carries and guides its orbiters on the long journey from Earth to Mercury.
  • E. Apollo command and service module
    The Apollo command and service module was the main crewed spacecraft used in NASA’s Apollo lunar missions, housing astronauts, life support, navigation, and propulsion systems for travel to and from the Moon.
  • F. None of above. chosen
  • G. Unsure - the case is ambiguous/there is not enough information to decide.
NEDg Description generation gpt-5.1
Instruction
Generate a one-sentence description of the target entity. 
You are given a context triple in the form (subject, predicate, object), where the object is the target entity. 
# Instructions
Use the triple to infer relevant information about the entity. Describe the entity based on what is most defining, well-known. 
Avoid repeating the information from the triple, unless really essential.
# Response Format
Return only the sentence: "Description: [one-sentence description of the target entity]"
Input
Entity: Saturn V instrument unit
Triple: [S-IC, guidanceSystemLocation, Saturn V instrument unit]
Generated description
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.
NED2 Entity disambiguation (via description) gpt-5-mini-2025-08-07
Target entity: Saturn V instrument unit
Target entity description: 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.
  • A. S-IVB
    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 IB
    Saturn IB was a two-stage American launch vehicle used by NASA in the 1960s and early 1970s to test Apollo spacecraft in Earth orbit and support missions such as Apollo–Soyuz.
  • D. Mercury Transfer Module
    The Mercury Transfer Module is the propulsion and support unit of the BepiColombo mission that carries and guides its orbiters on the long journey from Earth to Mercury.
  • E. Apollo command and service module
    The Apollo command and service module was the main crewed spacecraft used in NASA’s Apollo lunar missions, housing astronauts, life support, navigation, and propulsion systems for travel to and from the Moon.
  • F. None of above. chosen
PD Predicate disambiguation gpt-5-mini-2025-08-07
Target predicate: guidanceSystemLocation
Context triple: [S-IC, guidanceSystemLocation, Saturn V instrument unit]
  • A. locationInSystem
    Indicates that one entity is situated within or belongs to the spatial or organizational bounds of a particular system.
  • B. primaryGuidanceSystem
    Indicates that one entity functions as the main or principal guidance or navigation system for another entity.
  • C. navigationSystemComponent chosen
    Indicates that one entity functions as a component or subpart of a navigation system associated with another entity.
  • D. guidanceControl
    Indicates that one entity directs, manages, or influences the behavior or decisions of another through guidance or control.
  • E. coordinateLocation
    Indicates that an entity is located at, or associated with, a specific geographic coordinate or set of coordinates.
  • F. None of above.

Provenance (6 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_69c0084869e881908d7859492183ca7b completed March 22, 2026, 3:18 p.m.
NER Named-entity recognition batch_69c0400f1af881908d376ea4793f6dea completed March 22, 2026, 7:16 p.m.
NED1 Entity disambiguation (via context triple) batch_69c0a185cc78819098c0f04e7ebfb3c4 completed March 23, 2026, 2:12 a.m.
NEDg Description generation batch_69c0a2463cb08190aa5976ebd62c30d6 completed March 23, 2026, 2:15 a.m.
NED2 Entity disambiguation (via description) batch_69c0a2afcef88190a77c8089a1b85393 completed March 23, 2026, 2:17 a.m.
PD Predicate disambiguation batch_69c0333fdd7081908d829265caa2ac11 completed March 22, 2026, 6:21 p.m.
Created at: March 22, 2026, 3:53 p.m.