Triple
T2330384
| Position | Surface form | Disambiguated ID | Type / Status |
|---|---|---|---|
| Subject | GSLV Mk III |
E48387
|
entity |
| Predicate | thirdStageEngine |
P25128
|
FINISHED |
| Object |
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.
|
E256007
|
NE FINISHED |
Provenance (6 batches)
| Stage | Batch ID | Job type | Status |
|---|---|---|---|
| creating | batch_69a88aa308a88190b0b86c011fda7fce |
elicitation | completed |
| NER | batch_69abcc30c5e881908c5d526d7e7491d0 |
ner | completed |
| NED1 | batch_69ae8974ab8c81908ec2bddcc882cf42 |
ned_source_triple | completed |
| NED2 | batch_69ae8a895b6c8190bfd064742e3cc4f8 |
ned_description | completed |
| NEDg | batch_69ae8a084b388190a6d79df8d94b236d |
nedg | completed |
| PD | batch_69abc5926d048190a535e3f23d41de2a |
pd | completed |
Created at: March 4, 2026, 7:50 p.m.