L110 liquid core stage
E889639
The L110 liquid core stage is a cryogenic rocket stage used in India’s GSLV Mk III launch vehicle, providing the main liquid propulsion for its ascent.
All labels observed (1)
| Label | Occurrences |
|---|---|
| L110 liquid core stage canonical | 1 |
How this entity was disambiguated
This entity first appeared as the object of triple T10845847 — 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.
Target entity: L110 liquid core stage Context triple: [L110, fullName, L110 liquid core stage]
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A.
The Core Stage
The Core Stage is a major themed performance stage at the Tomorrowland electronic dance music festival, known for hosting prominent DJs and immersive audiovisual shows.
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B.
BE-3 engine
The BE-3 engine is a liquid hydrogen–liquid oxygen rocket engine developed by Blue Origin, best known for powering the company’s New Shepard suborbital launch vehicle.
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C.
BE-7 engine
The BE-7 engine is Blue Origin’s high-performance liquid hydrogen–liquid oxygen rocket engine designed primarily to power lunar landers such as the company’s Blue Moon vehicle.
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D.
Star 48BV upper stage
The Star 48BV upper stage is a solid-fueled rocket motor used as a high-energy kick stage to boost spacecraft, such as NASA’s Parker Solar Probe, onto their required trajectories.
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E.
Interim Cryogenic Propulsion Stage
The Interim Cryogenic Propulsion Stage is a liquid hydrogen–liquid oxygen upper stage used on early NASA Space Launch System missions to provide orbital insertion and translunar injection capability before the introduction of a more powerful exploration upper stage.
- F. None of above. chosen
- G. Unsure - the case is ambiguous/there is not enough information to decide.
Target entity: L110 liquid core stage Target entity description: The L110 liquid core stage is a cryogenic rocket stage used in India’s GSLV Mk III launch vehicle, providing the main liquid propulsion for its ascent.
-
A.
The Core Stage
The Core Stage is a major themed performance stage at the Tomorrowland electronic dance music festival, known for hosting prominent DJs and immersive audiovisual shows.
-
B.
BE-3 engine
The BE-3 engine is a liquid hydrogen–liquid oxygen rocket engine developed by Blue Origin, best known for powering the company’s New Shepard suborbital launch vehicle.
-
C.
BE-7 engine
The BE-7 engine is Blue Origin’s high-performance liquid hydrogen–liquid oxygen rocket engine designed primarily to power lunar landers such as the company’s Blue Moon vehicle.
-
D.
Star 48BV upper stage
The Star 48BV upper stage is a solid-fueled rocket motor used as a high-energy kick stage to boost spacecraft, such as NASA’s Parker Solar Probe, onto their required trajectories.
-
E.
Interim Cryogenic Propulsion Stage
The Interim Cryogenic Propulsion Stage is a liquid hydrogen–liquid oxygen upper stage used on early NASA Space Launch System missions to provide orbital insertion and translunar injection capability before the introduction of a more powerful exploration upper stage.
- F. None of above. chosen
Statements (48)
| Predicate | Object |
|---|---|
| instanceOf |
launch vehicle core stage
ⓘ
rocket stage ⓘ |
| burnTime | approximately 200 seconds ⓘ |
| controlSystem | hydraulic gimbal actuators ⓘ |
| countryOfOrigin | India ⓘ |
| developedBy |
LPSC
NERFINISHED
ⓘ
Liquid Propulsion Systems Centre NERFINISHED ⓘ |
| diameter | 4 meters ⓘ |
| engineArrangement | twin-engine ⓘ |
| engineType | Vikas engine NERFINISHED ⓘ |
| firstFlightVehicle | GSLV Mk III D1 NERFINISHED ⓘ |
| firstFlightYear | 2017 ⓘ |
| fuel |
UDMH
ⓘ
unsymmetrical dimethylhydrazine ⓘ |
| guidance | gimballed engines for thrust vector control ⓘ |
| isPartOf |
GSLV Mk III launch vehicle
NERFINISHED
ⓘ
LVM3 launch vehicle NERFINISHED ⓘ |
| launchPad | Second Launch Pad, SDSC NERFINISHED ⓘ |
| launchSite | Satish Dhawan Space Centre NERFINISHED ⓘ |
| launchVehicleConfiguration | two S200 boosters plus L110 core plus C25 upper stage ⓘ |
| launchVehicleFamily | Geosynchronous Satellite Launch Vehicle Mark III NERFINISHED ⓘ |
| length | approximately 21 meters ⓘ |
| lowerStage | S200 solid rocket booster ⓘ |
| manufacturer |
ISRO Propulsion Complex
NERFINISHED
ⓘ
Indian Space Research Organisation NERFINISHED ⓘ |
| missionProfilePhase | ascent phase main propulsion ⓘ |
| numberOfEngines | 2 ⓘ |
| operator | Indian Space Research Organisation ⓘ |
| oxidizer |
N2O4
ⓘ
nitrogen tetroxide ⓘ |
| propellantMass |
110 metric tons
ⓘ
110000 kilograms ⓘ |
| propellantType | hypergolic propellant ⓘ |
| propulsionType | liquid propulsion ⓘ |
| reusability | expendable ⓘ |
| stageRole |
core stage
ⓘ
second stage of GSLV Mk III ⓘ |
| status | operational ⓘ |
| structureMaterial | aluminium alloy ⓘ |
| successorTo | GS2 stage of GSLV Mk II NERFINISHED ⓘ |
| thrustAtSeaLevel | about 1600 kilonewtons ⓘ |
| thrustInVacuum | about 1800 kilonewtons ⓘ |
| upperStage | C25 cryogenic upper stage ⓘ |
| usedFor |
geostationary transfer orbit missions
ⓘ
high-energy orbit missions ⓘ orbital launch ⓘ |
| usedInRocket |
GSLV Mk III
NERFINISHED
ⓘ
LVM3 NERFINISHED ⓘ |
How these facts were elicited
The pipeline generated the facts above by prompting gpt-5.1 with this entity's name + description and the instruction below.
You are a knowledge base construction expert. Given a subject entity and a description of it, return factual statements that you know for the subject as a JSON list of dictionaries(triples), where keys must be "subject", "predicate" and "object". The number of facts may be very high, between 25 to 50 or more, for very popular subjects. For less popular subjects, the number of facts can be very low, like 5 or 10. # Requirements - If you don't know the subject at all, return an empty list. - If the subject is not a named entity, return an empty list. - Include at least one triple where predicate is "instanceOf". - Do not get too wordy. - Separate several objects into multiple triples with one object.
Subject: L110 liquid core stage Description of subject: The L110 liquid core stage is a cryogenic rocket stage used in India’s GSLV Mk III launch vehicle, providing the main liquid propulsion for its ascent.
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.