The Use of a Solar Electrojet Propulsion System for Jupiter Satellite Injection

Details The Use of a Solar Electrojet Propulsion System for Jupiter Satellite Injection The Use of a Solar Electrojet Propulsion System for Jupiter Satellite Injection

Mar 2002

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002cosre..40..186k&link_type=abstract

Cosmic Research, v. 40, Issue 2, p. 186-193 (2002).

Physics

Scientific paper

The problem of optimization of the interplanetary trajectory of flight for a multistage spacecraft with high- and low-thrust engines into the Jupiter satellite orbit is considered. Low-thrust engines (stationary plasma engines) are used on a heliocentric flight segment. Their operation is maintained with electric power supply from solar batteries. The principal feasibility of the realization of such a project is shown, and estimations of the mass of a spacecraft placed into Jupiter's satellite orbit are presented.

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