LE-5A
E1241823
UNEXPLORED
LE-5A is a Japanese liquid-fueled rocket engine developed by JAXA for use on H-II series launch vehicles.
All labels observed (1)
| Label | Occurrences |
|---|---|
| LE-5A canonical | 1 |
How this entity was disambiguated
This entity first appeared as the object of triple T16921143 — resolving that mention is where its identity was fixed. The disambiguator weighed these candidate entities and picked the highlighted one (or “None”, minting a new entity). This is how homonymy is resolved: the same surface form can point to different entities.
NED1
Entity disambiguation (via context triple)
gpt-5-mini-2025-08-07
Target entity: LE-5A Context triple: [LE-5B, predecessor, LE-5A]
-
A.
LE-5B
The LE-5B is a Japanese liquid-fueled cryogenic rocket engine developed by JAXA and Mitsubishi Heavy Industries for use on the upper stages of modern H-II series launch vehicles.
-
B.
LE-7A
The LE-7A is a Japanese liquid-fueled rocket engine used to power the core stage of the H-IIA family of launch vehicles.
-
C.
LE-9
The LE-9 is a next-generation liquid hydrogen–liquid oxygen rocket engine developed by Japan’s JAXA and Mitsubishi Heavy Industries for the core stage of the H3 launch vehicle, emphasizing high efficiency and cost-effective, reliable operation.
-
D.
LC-5
LC-5 is a historic launch complex at Cape Canaveral used for early U.S. crewed spaceflights during the Mercury program.
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E.
LC-36A
LC-36A is one of the launch pads at Cape Canaveral’s Launch Complex 36, historically used for Atlas rocket launches.
- F. None of above. chosen
- G. Unsure - the case is ambiguous/there is not enough information to decide.
NED2
Entity disambiguation (via description)
gpt-5-mini-2025-08-07
Target entity: LE-5A Target entity description: LE-5A is a Japanese liquid-fueled rocket engine developed by JAXA for use on H-II series launch vehicles.
-
A.
LE-5B
The LE-5B is a Japanese liquid-fueled cryogenic rocket engine developed by JAXA and Mitsubishi Heavy Industries for use on the upper stages of modern H-II series launch vehicles.
-
B.
LE-7A
The LE-7A is a Japanese liquid-fueled rocket engine used to power the core stage of the H-IIA family of launch vehicles.
-
C.
LE-9
The LE-9 is a next-generation liquid hydrogen–liquid oxygen rocket engine developed by Japan’s JAXA and Mitsubishi Heavy Industries for the core stage of the H3 launch vehicle, emphasizing high efficiency and cost-effective, reliable operation.
-
D.
LC-5
LC-5 is a historic launch complex at Cape Canaveral used for early U.S. crewed spaceflights during the Mercury program.
-
E.
LC-36A
LC-36A is one of the launch pads at Cape Canaveral’s Launch Complex 36, historically used for Atlas rocket launches.
- F. None of above. chosen
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.