electric pump-fed engine

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.

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Wikidata
electric pump-fed cycle
rocket engine, 
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Sweden, Tarshish, Dong Fang Hong 2, Ekran, 

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Location: KML, Cluster Map, Maps,

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  Rutherford ⓘ
  liquid-propellant rocket engine

Frameless

Type	Subtype	Date	Description	Notes	Source
class	rocket engine		Rutherford	electric pump-fed engine, liquid-propellant rocket,	Wikidata