Triple

T20814154
Position Surface form Disambiguated ID Type / Status
Subject Lockheed Martin X-33 E512390 entity
Predicate intendedEngineModel P17976 FINISHED
Object Rocketdyne XRS-2200 linear aerospike
The Rocketdyne XRS-2200 linear aerospike is an experimental rocket engine that uses a linear aerospike nozzle to maintain high efficiency across a wide range of altitudes, developed for advanced reusable launch vehicle concepts.
E1451455 NE FINISHED

How this triple was built (4 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: Rocketdyne XRS-2200 linear aerospike | Statement: [Lockheed Martin X-33, intendedEngineModel, Rocketdyne XRS-2200 linear aerospike]
NED1 Entity disambiguation (via context triple) gpt-5-mini-2025-08-07
Target entity: Rocketdyne XRS-2200 linear aerospike
Context triple: [Lockheed Martin X-33, intendedEngineModel, Rocketdyne XRS-2200 linear aerospike]
  • A. 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.
  • B. Raptor engine
    The Raptor engine is SpaceX’s next-generation full-flow staged combustion methane-fueled rocket engine designed to power the Starship launch system.
  • C. NK-33 engine
    The NK-33 engine is a Soviet-era high-performance liquid-fuel rocket engine originally developed for the N1 lunar rocket program, known for its efficiency and thrust-to-weight ratio.
  • D. Rocketdyne H-1
    The Rocketdyne H-1 was a kerosene/liquid-oxygen rocket engine developed in the United States and used on early Saturn launch vehicles during the Apollo era.
  • E. RocketMotorOne
    RocketMotorOne is the hybrid rocket engine that powered the experimental suborbital spaceplane SpaceShipOne on its historic private spaceflights.
  • 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: Rocketdyne XRS-2200 linear aerospike
Triple: [Lockheed Martin X-33, intendedEngineModel, Rocketdyne XRS-2200 linear aerospike]
Generated description
The Rocketdyne XRS-2200 linear aerospike is an experimental rocket engine that uses a linear aerospike nozzle to maintain high efficiency across a wide range of altitudes, developed for advanced reusable launch vehicle concepts.
NED2 Entity disambiguation (via description) gpt-5-mini-2025-08-07
Target entity: Rocketdyne XRS-2200 linear aerospike
Target entity description: The Rocketdyne XRS-2200 linear aerospike is an experimental rocket engine that uses a linear aerospike nozzle to maintain high efficiency across a wide range of altitudes, developed for advanced reusable launch vehicle concepts.
  • A. 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.
  • B. Raptor engine
    The Raptor engine is SpaceX’s next-generation full-flow staged combustion methane-fueled rocket engine designed to power the Starship launch system.
  • C. NK-33 engine
    The NK-33 engine is a Soviet-era high-performance liquid-fuel rocket engine originally developed for the N1 lunar rocket program, known for its efficiency and thrust-to-weight ratio.
  • D. Rocketdyne H-1
    The Rocketdyne H-1 was a kerosene/liquid-oxygen rocket engine developed in the United States and used on early Saturn launch vehicles during the Apollo era.
  • E. RocketMotorOne
    RocketMotorOne is the hybrid rocket engine that powered the experimental suborbital spaceplane SpaceShipOne on its historic private spaceflights.
  • F. None of above. chosen

Provenance (5 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_69e0b4cd25088190b48ca9700cd24efc completed April 16, 2026, 10:07 a.m.
NER Named-entity recognition batch_69e6c2d4e43c8190aecce82a3f7e2de0 completed April 21, 2026, 12:20 a.m.
NED1 Entity disambiguation (via context triple) batch_6a08f8cdb5d08190a8925efe00fef10e completed May 16, 2026, 11:07 p.m.
NEDg Description generation batch_6a08f9f7aff481908283ffe92d95646d completed May 16, 2026, 11:12 p.m.
NED2 Entity disambiguation (via description) batch_6a08faa15c488190b7a3ed000c093be7 completed May 16, 2026, 11:15 p.m.
Created at: April 16, 2026, 12:40 p.m.