Triple

T6140271
Position Surface form Disambiguated ID Type / Status
Subject LR-91 E136942 entity
Predicate usedOnVariant P39014 FINISHED
Object Titan II GLV E80654 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: Titan II GLV | Statement: [LR-91, usedOnVariant, Titan II GLV]
NED1 Entity disambiguation (via context triple) gpt-5-mini-2025-08-07
Target entity: Titan II GLV
Context triple: [LR-91, usedOnVariant, Titan II GLV]
  • A. Titan II GLV chosen
    Titan II GLV was a modified two-stage Titan II intercontinental ballistic missile used by NASA as the launch vehicle for all crewed Gemini spacecraft during the mid-1960s.
  • B. Titan IIIE
    Titan IIIE was a U.S. expendable launch vehicle variant of the Titan III family, equipped with a Centaur upper stage and used in the 1970s to send deep-space probes such as Voyager 1 on interplanetary trajectories.
  • C. Titan III
    Titan III was a family of American expendable launch vehicles developed during the Cold War era to support heavy military and civilian payloads into Earth orbit and beyond.
  • D. Atlas II
    Atlas II was an American expendable launch vehicle family developed by General Dynamics and later Lockheed Martin, used primarily in the 1990s to launch commercial and military satellites into orbit.
  • E. Titan II second stage
    The Titan II second stage was the upper propulsion segment of the Titan II launch vehicle used during the Gemini program, serving as the spent target object for early U.S. crewed orbital rendezvous attempts.
  • 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_69c008a179388190a3b5a081bbf46d55 completed March 22, 2026, 3:20 p.m.
NER Named-entity recognition batch_69c05cb030fc8190b78e4967eea65611 completed March 22, 2026, 9:18 p.m.
NED1 Entity disambiguation (via context triple) batch_69c135ecd62c8190911b98133bf71dfc completed March 23, 2026, 12:45 p.m.
Created at: March 22, 2026, 4:15 p.m.