Fig. 5.

Payload accommodation on Solar Orbiter S/C. The RPW sub-units are indicated in red. The electric Antenna system (ANT) consists of a set of three identical antennas deployed from +Z axis (Antenna PZ) and from the opposite corners of the S/C +Y and -Y walls (Antennas PY and MY). The SCM consists of a set of three magnetic antennas mounted orthogonally. Their orientations, in the S/C reference frame, are given by the three vectors in the upper left part of the figure. Finally the Main Electronic Box (MEB) is located inside the S/C body.
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.