Triple
T13538567
| Position | Surface form | Disambiguated ID | Type / Status |
|---|---|---|---|
| Subject | International Habitation Module |
E323322
|
entity |
| Predicate | connectedTo |
P37
|
FINISHED |
| Object | Gateway Power and Propulsion Element |
E323321
|
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: Gateway Power and Propulsion Element | Statement: [International Habitation Module, connectedTo, Gateway Power and Propulsion Element]
NED1
Entity disambiguation (via context triple)
gpt-5-mini-2025-08-07
Target entity: Gateway Power and Propulsion Element Context triple: [International Habitation Module, connectedTo, Gateway Power and Propulsion Element]
-
A.
Power and Propulsion Element
chosen
The Power and Propulsion Element is a planned NASA spacecraft module that will provide solar electric propulsion, power, and communications for the Lunar Gateway space station in lunar orbit.
-
B.
Rutherford engine
The Rutherford engine is a small, electric-pump-fed liquid rocket engine developed by Rocket Lab for its Electron launch vehicle, notable for being 3D-printed and highly efficient for small-satellite launches.
-
C.
Service Propulsion System (SPS)
The Service Propulsion System (SPS) was the main liquid-fueled rocket engine of the Apollo Service Module, used for major course corrections, lunar orbit insertion, and trans-Earth injection during Apollo missions.
-
D.
Peacekeeper post-boost propulsion system
The Peacekeeper post-boost propulsion system is the maneuvering and guidance stage of the Peacekeeper ICBM that precisely deploys multiple reentry vehicles onto their designated targets after the main boost phase.
-
E.
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.
- 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_69d8076776248190bdf0d4fa1f85a5fc |
completed | April 9, 2026, 8:09 p.m. |
| NER | Named-entity recognition | batch_69dbafd7ad9481908fe1d7ffcf8fab71 |
completed | April 12, 2026, 2:44 p.m. |
| NED1 | Entity disambiguation (via context triple) | batch_69f75d9c04b881908a359df791b89b43 |
completed | May 3, 2026, 2:37 p.m. |
Created at: April 9, 2026, 9:45 p.m.