EPSC Abstracts
Vol. 17, EPSC2024-703, 2024, updated on 03 Jul 2024
https://doi.org/10.5194/epsc2024-703
Europlanet Science Congress 2024
© Author(s) 2024. This work is distributed under
the Creative Commons Attribution 4.0 License.
Poster | Wednesday, 11 Sep, 10:30–12:00 (CEST), Display time Wednesday, 11 Sep, 08:30–19:00|

M-MATISSE MaCro: an intersatellite link in Mars orbit

Pätzold Martin1, Tom Andert2, Takeshi Imamura3, Hiroki Ando4, Antonio Genova5, Matthias Hahn1, Katsuyuki Noguchi6, Janusz Oschlisniok1, Kerstin Peter1, Silvia Tellmann1, Beatriz Sanchez-Cano7, and Francois Leblanc8
Pätzold Martin et al.
  • 1Rheinisches Institut für Umweltforschung an der Universität zu Köln, Abteilung Planetenforschung, Germany (martin.paetzold@uni-koeln.de)
  • 2Institut für Raumfahrttechnik und Weltraumnutzung, Universität der Bundeswehr München, Neubiberg, Germany
  • 3Graduate School of Frontier Sciences, The University of Tokyo, Tokyo, Japan
  • 4Kyoto Sangyo University, Kyoto, Japan
  • 5Department of Mechanical and Aerospace Enginnering, Universita di Roma, Rome, Italy
  • 6Womens University Nara, Nara, Japan
  • 7School of Physics and Astronomy, University of Leicester, Leicester, UK
  • 8LATMOS, Sorbonne Universite, Paris, France

The "Mars Magnetosphere ATmosphere Ionosphere and Space-weather SciencE (M-MATISSE)" mission, currently in Phase A study by the European Space Agency (ESA), is a Medium-class (M7) candidate. M-MATISSE aims to unravel the intricate and dynamic couplings of the Martian magnetosphere, ionosphere, and thermosphere (MIT coupling) in relation to the solar wind (i.e., space weather) and the lower atmosphere. This two-spacecraft mission involves both spacecraft carrying an identical payload suite, each following different orbits with an apocenter at 3,000 km and 10,000 km altitude, and a pericenter at 250 km altitude. The intersatellite radio link, MaCro, operates at two frequencies to probe the ionosphere and atmosphere of Mars during occultations, as one spacecraft disappears behind the planetary disk as seen from the other spacecraft. The instrumentation comprises two transceivers at UHF and S-band, stabilized by an ultrastable oscillator on both spacecraft each. The observables include the shift of the carrier frequencies caused by the bending of the radio ray path in the atmosphere/ionosphere. Onboard data pre-processing precedes the transmission of telemetry to Earth. The orbits allow about eight occultations events (ingress or egress) on average per day starting at an altitude of 1000 km.

How to cite: Martin, P., Andert, T., Imamura, T., Ando, H., Genova, A., Hahn, M., Noguchi, K., Oschlisniok, J., Peter, K., Tellmann, S., Sanchez-Cano, B., and Leblanc, F.: M-MATISSE MaCro: an intersatellite link in Mars orbit, Europlanet Science Congress 2024, Berlin, Germany, 8–13 Sep 2024, EPSC2024-703, https://doi.org/10.5194/epsc2024-703, 2024.