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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electric pump-fed cycle
rocket engine, 
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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  Rutherford ⓘ
  liquid-propellant rocket engine

Frameless

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