Low-Cost Interplanetary Missions Using Electric Propulsion

A. R. Martin, W. E. F. L. Moulford. (1996), JBIS, 49, pp.447-545

Refcode: 1996.49.447

Abstract:

Interplanetary science missions often require a significant propulsive capability over and above that provided by the launch vehicle. Examples are in-course velocity increments to reduce trip time, trajectory modifications, or propulsion burns to rendezvous with the target.