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Electric Propulsion For Low Earth Orbit Constellations by jonathan.hilton is a document available to read on EtoBox.
The document evaluates the use of Hall Effect electric propulsion for low Earth orbit (LEO) satellite constellations, highlighting its advantages over chemical propulsion, particularly in terms of increased payload capacity and reduced launch vehicle requirements. It discusses mission analysis, options, and assumptions, including the ability to reposition satellites and maintain orbits using electric propulsion systems. The findings suggest that using electric propulsion can significantly lower the number o
- Author
- jonathan.hilton
- Language
- EN