Triple

T10846026
Position Surface form Disambiguated ID Type / Status
Subject Gaganyaan test missions E256010 entity
Predicate technologyTested P60540 FINISHED
Object Crew Escape System E323526 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: Crew Escape System | Statement: [Gaganyaan test missions, technologyTested, Crew Escape System]
NED1 Entity disambiguation (via context triple) gpt-5-mini-2025-08-07
Target entity: Crew Escape System
Context triple: [Gaganyaan test missions, technologyTested, Crew Escape System]
  • A. Martin-Baker ejection seats
    Martin-Baker ejection seats are British-designed emergency escape systems used in military aircraft worldwide to safely propel aircrew out of a stricken aircraft.
  • B. HL-20 Personnel Launch System
    The HL-20 Personnel Launch System was a NASA-designed lifting-body spaceplane concept from the late 20th century intended to provide a reusable, crewed vehicle for low Earth orbit missions and runway landings.
  • C. Orion Launch Abort System chosen
    The Orion Launch Abort System is a safety system designed to rapidly pull NASA’s Orion crew capsule away from its rocket in the event of an emergency during launch or ascent.
  • D. Quest Joint Airlock
    The Quest Joint Airlock is the primary airlock module of the International Space Station, used for conducting U.S. and partner spacewalks.
  • E. Orbital Maneuvering System
    The Orbital Maneuvering System was the Space Shuttle’s pair of rear-mounted rocket engines used for orbital insertion, adjustment, and deorbit burns.
  • 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_69d6aa81a5d08190aa86689061d1ddd2 completed April 8, 2026, 7:20 p.m.
NER Named-entity recognition batch_69d750d132e081909c977b3dc4110ca4 completed April 9, 2026, 7:10 a.m.
NED1 Entity disambiguation (via context triple) batch_69deb162d718819081fbc3a082672b4f completed April 14, 2026, 9:28 p.m.
Created at: April 8, 2026, 9:19 p.m.