2020
DOI: 10.1007/s11214-020-00760-0
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The MEFISTO and WPT Electric Field Sensors of the Plasma Wave Investigation on the BepiColombo Mio Spacecraft

Abstract: This paper describes the design of MEFISTO (Mercury Electric Field In-Situ Tool) and WPT (Wire Probe Antenna) electric field sensors for Plasma Wave Investigation (PWI) on the BepiColombo Mio spacecraft (Mercury Magnetospheric Orbiter, MMO). The two sensors will enable the first observations of electric fields, plasma waves and radio waves in and around the Hermean magnetosphere and exosphere. MEFISTO and WPT are dipole antennas with 31.6 m tip-to-tip length. Each antenna element has a spherical probe at each … Show more

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Cited by 8 publications
(5 citation statements)
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“…At the same time, the spacecraft carries a variety of magnetic field and electric field instruments, including the magnetometer, i.e., MPO/MAG (Glassmeier et al, 2010;Heyner et al, 2021) and Mio/MGF (Baumjohann et al, 2020). In particular, Mio/Plasma wave experiment (PWI) will provide the first electric field measurements from DC to 10 MHz (Karlsson et al, 2020;Kasaba et al, 2020), and search coil magnetometers with frequency up to 20 kHz (Yagitani et al, 2020). With these high sampling rate for magnetic field and electric field measurements, we can better understand the electromagnetic field waves and plasma waves in Mercury's magnetosphere and further our investigations of wave-particle interactions and the energetic particle environment of Mercury.…”
Section: Future Bepicolombo Opportunitiesmentioning
confidence: 99%
“…At the same time, the spacecraft carries a variety of magnetic field and electric field instruments, including the magnetometer, i.e., MPO/MAG (Glassmeier et al, 2010;Heyner et al, 2021) and Mio/MGF (Baumjohann et al, 2020). In particular, Mio/Plasma wave experiment (PWI) will provide the first electric field measurements from DC to 10 MHz (Karlsson et al, 2020;Kasaba et al, 2020), and search coil magnetometers with frequency up to 20 kHz (Yagitani et al, 2020). With these high sampling rate for magnetic field and electric field measurements, we can better understand the electromagnetic field waves and plasma waves in Mercury's magnetosphere and further our investigations of wave-particle interactions and the energetic particle environment of Mercury.…”
Section: Future Bepicolombo Opportunitiesmentioning
confidence: 99%
“…However, the physics at these scales is exactly one of the main scientific objectives of the ongoing ESA/JAXA space mission BepiColombo (Benkhoff et al 2010). Different plasma instruments onboard the Mio spacecraft will provide measurements of: (i) the plasma density profile along the spacecraft trajectory, using different complementary experiments, namely, Langmuir probe measurements (Karlsson et al 2020), quasi-thermal noise measurements (Moncuquet et al 2006), and mutual impedance measurements (Gilet et al 2019), all within the Plasma Wave Investigation (PWI) consortium (Kasaba et al 2020), (ii) the electric field in the lower-hybrid frequency range (PWI), and (iii) the electron distribution function (MPPE/MEA, Mercury Plasma Particle Experiment and Mercury Electron Analyzer (Saito et al 2010)). This will enable us to directly address the physics of Mercury's strongly inhomogeneous magnetopause.…”
Section: Application To Mercury's Magnetopausementioning
confidence: 99%
“…This means that we expect, at least for a significant part of the mission, a plasma sheath characterized by a local excess of electrons. The size of such plasma sheath shall be of the order of the Debye length λ D that is expected to be in the range 1–10 m in the plasma environment of Mercury, while the electric sensors (the MEFISTO antennas (Karlsson et al., 2020)) are 15 m long. Our investigation indicates that one has to include the plasma sheath of the Mio spacecraft in the modeling and the analysis of PWI‐AM2P spectra to retrieve satisfactorily the electron temperature.…”
Section: Discussionmentioning
confidence: 99%
“…This is the case for the PWI‐AM2P instrument onboard the Mio spacecraft of the BepiColombo mission. PWI‐AM2P uses two emitting and two receiving electric antennas installed on four 15 m wires (Karlsson et al., 2020) and the local Debye length is expected to range between 1 and 10 m in Mercury's magnetosphere (Kasaba et al., 2010). Hence, Debye length encountered by PWI‐AM2P is not always expected to be negligible with respect to the distance between MI electric sensors.…”
Section: Introductionmentioning
confidence: 99%