Deep Space One (DSI) is the first interplanetary spacecraft operated on sol
ar electric propulsion. One of the primary investigations of DSI is to char
acterize ion propulsion-induced plasma interactions and their effects on sp
acecraft and solar wind measurements based on two plasma diagnostic package
s. The first in situ measurements of an ion propulsion-induced plasma envir
onment obtained from an interplanetary spacecraft are reported. Analysis of
the measurements reveals interesting correlations between the induced char
ge-exchange plasma environment and thruster operating conditions. Sensors n
ear the thruster exit measured charge-exchange ions with a number density o
f similar to 10(6) cm(-3) and a current density of similar to 10(-7) A/cm(-
2) under typical thruster operating conditions, a result in good agreement
with preflight predictions based on computer particle simulations. Observat
ions on the opposite side from the thruster suggest that the dominant facto
r for charge-exchange ion backflow is the potential distribution surroundin
g the spacecraft rather than the charge-exchange ion production rate.