It is considered the possibility to use the stationary plasma (Hall) t
hrusters for the Pluto fast flyby mission [1-3]. There were considered
applications of the existing and working out space technology compone
nts, such as Russian launcher Proton, upper stage Block D (Block DM),
series M100-M290 of SPT [4-6], Germany and US solar arrays [4, 5]. The
re were considered direct flight to Pluto and Jupiter swingby trajecto
ries. This investigation demonstrates the possibility to realize a Plu
to fast flyby mission based on considered thrusters and solar electric
al power unit. Use of solar electric propulsion allows a decrease of t
ransfer time, and increased mass of payload.