Q28454000: Difference between revisions
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Q28454000
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{{Page|electric pump-fed engine|Classes|rocket engine using an electric pump for pressurization}} | {{Page|electric pump-fed engine|Classes|rocket engine using an electric pump for pressurization|electric pump-fed cycle}} | ||
Latest revision as of 15:58, 17 February 2025
The electric-pump-fed engine is a bipropellant rocket engine in which the fuel pumps are electrically powered, and so all of the input propellant is directly burned in the main combustion chamber, and none is diverted to drive the pumps. This differs from traditional rocket engine designs, in which the pumps are driven by a portion of the input propellants.
Wikidata
electric pump-fed cycle
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, rocket engine, Rutherford, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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Rutherford ⓘ
liquid-propellant rocket engine
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| class | rocket engine | Rutherford | liquid-propellant rocket, electric pump-fed engine | Wikidata | |