2020
DOI: 10.1029/2019ja027544
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The Shape of Mercury's Magnetopause: The Picture From MESSENGER Magnetometer Observations and Future Prospects for BepiColombo

Abstract: The MErcury Surface, Space Environment, GEochemistry, and Ranging (MESSENGER) spacecraft orbited Mercury between March 2011 and April 2015, typically passing through the magnetosphere, magnetosheath, and interplanetary magnetic field, on each orbit. Using data from the Magnetometer, we identify magnetopause crossings for the complete orbital mission and model the average boundary shape. We find that Mercury's average magnetopause is well modeled by both an axisymmetric shape and a three-dimensional shape co… Show more

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Cited by 23 publications
(34 citation statements)
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“…It is important to note, that Zhong et al (2015a) calculated their error using only 1σ . Recently, Philpott et al (2020) cast some doubt about the shape of the cusp indentions. Figure 14 shows a comparison of the subsolar magnetopause distance as a function of heliocentric distance of Mercury derived from the three magnetopause models mentioned above.…”
Section: Hermean Magnetopausementioning
confidence: 99%
“…It is important to note, that Zhong et al (2015a) calculated their error using only 1σ . Recently, Philpott et al (2020) cast some doubt about the shape of the cusp indentions. Figure 14 shows a comparison of the subsolar magnetopause distance as a function of heliocentric distance of Mercury derived from the three magnetopause models mentioned above.…”
Section: Hermean Magnetopausementioning
confidence: 99%
“…To achieve this goal, accurate magnetic field measurements are thus of crucial importance. Therefore, the components of a linear calibration matrix M and an offset vector O need to be obtained, in order to convert raw instrument outputs B raw to fully calibrated magnetic field measurements (see for example Kepko et al, 1996;Plaschke and Narita, 2016):…”
Section: Introductionmentioning
confidence: 99%
“…Here, the matrix M transforms B raw into a spacecraft-fixed orthogonal coordinate system. It comprises nine parameters: three scaling (gain) values of the sensor and an orthogonalization matrix, which is defined by the three angles that yield the magnetometer sensor directions with respect to the spacecraft reference frame (see for example Plaschke and Narita, 2016). The 3D offset vector O, on the other hand, reflects the magnetometer outputs in vanishing ambient fields.…”
Section: Introductionmentioning
confidence: 99%
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