The Institute of Space and Astronautical Science (ISAS) launches the e
ngineering test spacecraft, MUSES-C toward a near Earth asteroid NEREU
S (4660) in 2002. It is aiming at demonstrating four key technologies
requisite for the future sample and return missions from extra terrest
rial bodies. They are 1) An electrical propulsion, ion thrusters in in
terplanetary field as a primary propulsive means, 2) An autonomous gui
dance and navigation based on optical aid, 3) An automated sampling me
chanism and 4) A direct hyperbolic reentry of the recovery capsule to
the ground. This paper presents the current design status of MUSES-C f
ocusing its attention on the contents and readiness of above mentioned
key technologies. Copyright (C) 1997 Elsevier Science Ltd.