Abstract This paper makes an updated assessment of the technical and economic feasibility of transferring satellites from low Earth orbit to geostationary orbit using low thrust propulsion. In particular, the concept of a solar electric tug is discussed whereby the main propulsion unit is returned from geostationary orbit to low Earth orbit for re-use.
A reappraisal of satellite orbit raising by electric propulsion
Acta Astronautica ; 19 , 6-7 ; 535-538
1989-02-15
4 pages
Article (Journal)
Electronic Resource
English