Triple

T2975513
Position Surface form Disambiguated ID Type / Status
Subject Mitsubishi J8M E80384 entity
Predicate powerplantModel P41535 FINISHED
Object Toku Ro.2 (KR10) rocket engine
The Toku Ro.2 (KR10) rocket engine was a Japanese liquid-fueled rocket motor developed in World War II to power interceptor aircraft such as the Mitsubishi J8M.
E316066 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: Toku Ro.2 (KR10) rocket engine | Statement: [Mitsubishi J8M, powerplantModel, Toku Ro.2 (KR10) rocket engine]
NED1 Entity disambiguation (via context triple) gpt-5-mini-2025-08-07
Target entity: Toku Ro.2 (KR10) rocket engine
Context triple: [Mitsubishi J8M, powerplantModel, Toku Ro.2 (KR10) rocket engine]
  • A. R-1 rocket
    The R-1 rocket was an early Soviet ballistic missile and research rocket developed after World War II as a near-copy of Germany’s V-2, serving as a foundation for later Soviet rocketry.
  • B. Walter rocket engine
    The Walter rocket engine was a German World War II-era liquid-fuel rocket propulsion system, best known for powering the Messerschmitt Me 163 Komet interceptor and pioneering high-thrust, short-duration flight technology.
  • C. Curtiss-Wright XLR25 rocket engine
    The Curtiss-Wright XLR25 was an American liquid-fueled rocket engine developed in the 1950s to power high-speed experimental research aircraft such as the Bell X-2.
  • D. RS-68 engine
    The RS-68 engine is a powerful liquid-fueled rocket engine used primarily on the Delta IV launch vehicle, known for its high thrust and simplified design for cost-effective heavy-lift missions.
  • E. RD-107
    RD-107 is a Soviet-designed liquid-fueled rocket engine, best known for powering the first stages of early R-7 family launch vehicles used in historic missions like Sputnik and Vostok.
  • 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: Toku Ro.2 (KR10) rocket engine
Triple: [Mitsubishi J8M, powerplantModel, Toku Ro.2 (KR10) rocket engine]
Generated description
The Toku Ro.2 (KR10) rocket engine was a Japanese liquid-fueled rocket motor developed in World War II to power interceptor aircraft such as the Mitsubishi J8M.
NED2 Entity disambiguation (via description) gpt-5-mini-2025-08-07
Target entity: Toku Ro.2 (KR10) rocket engine
Target entity description: The Toku Ro.2 (KR10) rocket engine was a Japanese liquid-fueled rocket motor developed in World War II to power interceptor aircraft such as the Mitsubishi J8M.
  • A. R-1 rocket
    The R-1 rocket was an early Soviet ballistic missile and research rocket developed after World War II as a near-copy of Germany’s V-2, serving as a foundation for later Soviet rocketry.
  • B. Walter rocket engine
    The Walter rocket engine was a German World War II-era liquid-fuel rocket propulsion system, best known for powering the Messerschmitt Me 163 Komet interceptor and pioneering high-thrust, short-duration flight technology.
  • C. Curtiss-Wright XLR25 rocket engine
    The Curtiss-Wright XLR25 was an American liquid-fueled rocket engine developed in the 1950s to power high-speed experimental research aircraft such as the Bell X-2.
  • D. RS-68 engine
    The RS-68 engine is a powerful liquid-fueled rocket engine used primarily on the Delta IV launch vehicle, known for its high thrust and simplified design for cost-effective heavy-lift missions.
  • E. RD-107
    RD-107 is a Soviet-designed liquid-fueled rocket engine, best known for powering the first stages of early R-7 family launch vehicles used in historic missions like Sputnik and Vostok.
  • F. None of above. chosen
PD Predicate disambiguation gpt-5-mini-2025-08-07
Target predicate: powerplantModel
Context triple: [Mitsubishi J8M, powerplantModel, Toku Ro.2 (KR10) rocket engine]
  • A. powerplantVariant chosen
    Indicates that one power plant is a specific version, configuration, or model variant of another power plant design.
  • B. powerplant
    Indicates that an entity functions as a facility or installation where energy sources are converted into usable power, typically electricity.
  • C. powerplantFor
    Indicates that one entity functions as the power plant or primary energy source serving another entity.
  • D. powerplantType
    Indicates the specific kind or category of power plant associated with an entity, based on how it generates energy.
  • E. powerplantManufacturer
    Indicates that one entity is the company or organization responsible for manufacturing or producing the power plant associated with another entity.
  • 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_69ad8b14ffe881908ffed62f9595c867 completed March 8, 2026, 2:43 p.m.
NER Named-entity recognition batch_69ad998ad5308190a012ec4940eb46cb completed March 8, 2026, 3:45 p.m.
NED1 Entity disambiguation (via context triple) batch_69b108e99ea881908cccc6656e8653c3 completed March 11, 2026, 6:17 a.m.
NEDg Description generation batch_69b109fc0f308190b1a0105a67491c54 completed March 11, 2026, 6:21 a.m.
NED2 Entity disambiguation (via description) batch_69b10a78414481908689ac3ba5265388 completed March 11, 2026, 6:23 a.m.
PD Predicate disambiguation batch_69ad96105a708190a9ec4838cbcb1207 completed March 8, 2026, 3:30 p.m.
Created at: March 8, 2026, 2:58 p.m.