page_title: CE-20
hierarchical_section_title: CE-20
caption_attribution_description: English: A computer model of CE-20 LH2/LOX cryogenic rocket engine developed by Indian Space Research Organisation for use in the GSLV Mk III orbital rocket. Français&#160;: Un modèle informatique du moteur de fusée cryogénique CE-20 LH2 / LOX développé par Organisation indienne pour la recherche spatiale pour une utilisation dans la fusée GSLV Mk III.
context_page_description: The CE-20 is a cryogenic rocket engine developed by the Liquid Propulsion Systems Centre, a subsidiary of Indian Space Research Organisation. It has been developed to power the upper stage of the Geosynchronous Satellite Launch Vehicle Mk III. It is the first Indian cryogenic engine to feature a gas-generator cycle. The high thrust cryogenic engine is one of
  the most powerful upper stage cryogenic engines in the world.
context_section_description: The CE-20 is a cryogenic rocket engine developed by the Liquid Propulsion Systems Centre, a subsidiary of Indian Space Research Organisation. It has been developed to power the upper stage of the Geosynchronous Satellite Launch Vehicle Mk III. It is the first Indian cryogenic engine to feature a gas-generator cycle. The high thrust cryogenic engine is one of
  the most powerful upper stage cryogenic engines in the world.
caption: A computer model of CE-20
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