Q28454000: Difference between revisions
From Spacefaring
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
Reman, Republic of Haiti, Rutherford, rocket engine, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Sikh Confederacy, Ashkenaz, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent,
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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 | |