CE-20
id:
ce-20-248-1380420
title:
CE-20
text:
The CE-20 is a cryogenic rocket engine developed by the Liquid Propulsion Systems Centre (LPSC), a subsidiary of the Indian Space Research Organisation (ISRO). It has been developed to power the upper stage of the LVM3. It is the first Indian cryogenic engine to feature a gas-generator cycle. The high thrust cryogenic engine is the most powerful upper stage cryogenic engine in operational service.
brand slug:
wiki
category slug:
encyclopedia
description:
Rocket engine developed by ISRO for upper stage of its GSLV Mk III rocket
original url:
https://en.wikipedia.org/wiki/CE-20
date created:
date modified:
2024-03-26T19:54:12Z
main entity:
{"identifier":"Q4272906","url":"https://www.wikidata.org/entity/Q4272906"}
image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/3/37/CE-20_Engine_Config_Model.png","width":529,"height":524}
fields total:
13
integrity:
15