NEXT-C ion thruster
E1181937
UNEXPLORED
The NEXT-C ion thruster is a high-efficiency NASA-developed electric propulsion system designed for deep-space missions, providing continuous low-thrust acceleration using ionized xenon.
All labels observed (1)
| Label | Occurrences |
|---|---|
| NEXT-C ion thruster canonical | 1 |
How this entity was disambiguated
This entity first appeared as the object of triple T15880780 — 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: NEXT-C ion thruster Context triple: [DART spacecraft, propulsion, NEXT-C ion thruster]
-
A.
Hall-effect thrusters
Hall-effect thrusters are a type of electric propulsion system for spacecraft that use magnetic and electric fields to accelerate ions and produce efficient, low-thrust propulsion for orbital maneuvers and deep-space missions.
-
B.
CE-20 cryogenic engine
The CE-20 cryogenic engine is an Indian-developed, liquid hydrogen–liquid oxygen rocket engine that powers the upper stage of ISRO’s heaviest launch vehicles for placing large payloads into orbit.
-
C.
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.
-
D.
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.
-
E.
Titan propulsion system family
The Titan propulsion system family is a series of liquid-fueled rocket engines and stages developed for the U.S. Titan launch vehicles, used extensively for military missiles and space launch missions during the Cold War and beyond.
- 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: NEXT-C ion thruster Target entity description: The NEXT-C ion thruster is a high-efficiency NASA-developed electric propulsion system designed for deep-space missions, providing continuous low-thrust acceleration using ionized xenon.
-
A.
Hall-effect thrusters
Hall-effect thrusters are a type of electric propulsion system for spacecraft that use magnetic and electric fields to accelerate ions and produce efficient, low-thrust propulsion for orbital maneuvers and deep-space missions.
-
B.
CE-20 cryogenic engine
The CE-20 cryogenic engine is an Indian-developed, liquid hydrogen–liquid oxygen rocket engine that powers the upper stage of ISRO’s heaviest launch vehicles for placing large payloads into orbit.
-
C.
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.
-
D.
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.
-
E.
Titan propulsion system family
The Titan propulsion system family is a series of liquid-fueled rocket engines and stages developed for the U.S. Titan launch vehicles, used extensively for military missiles and space launch missions during the Cold War and beyond.
- F. None of above. chosen
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.