1. Introduction
The sample return mission, Martian Moons eXploration (MMX), of the Japan Aerospace Agency (JAXA) carries a rover on its way, which will be deployed as a scout on Phobos to perform several scientific tasks during the mission. The deployment aims to ballistically descend the MMX rover on the surface of Phobos and start with its scientific objectives after uprighting with the MMX Rover's Locomotion Sub-system (LSS). The latter is a contribution by the Robotics and Mechatronics Center (RMC) of the German Aerospace Center (DLR) and objective of this paper. The subsystem is an integral part of the MMX rover and provides the link to interact physically with the surface of Phobos in milli-g environment. Not only is it a technical demonstration for driving at low gravity, in addition it serves as a sunpointing device for the solar arrays and supports multiple scientific objectives: e.g. the positioning of the internal scientific payload relative to the surface of Phobos or the direct interaction of the surface regolith to give informations on its characteristics.