scholarly journals The Energetic Particle Detector (EPD) Investigation and the Energetic Ion Spectrometer (EIS) for the Magnetospheric Multiscale (MMS) Mission

2014 ◽  
Vol 199 (1-4) ◽  
pp. 471-514 ◽  
Author(s):  
B. H. Mauk ◽  
J. B. Blake ◽  
D. N. Baker ◽  
J. H. Clemmons ◽  
G. D. Reeves ◽  
...  
2021 ◽  
Author(s):  
Javier Rodriguez-Pacheco ◽  

<p>In this presentation, we will show the first measurements performed by EPD since the end of the commissioning phase until the latest results obtained. During these months EPD has been scanning the inner heliosphere at different heliocentric distances and heliolongitues allowing - together with other spacecraft - to investigate the spatio-temporal behavior of the particle populations in the inner heliosphere during solar minimum conditions. Solar Orbiter was launched from Cape Canaveral on February 10th, 2020, thus beginning the journey to its encounter with the Sun. Solar Orbiter carries ten scientific instruments, six remote sensing and four in situ, that will allow the mission main goal: how the Sun creates and controls the heliosphere. Among the in situ instruments, the Energetic Particle Detector (EPD) measures electrons, protons and heavy ions with high temporal resolution over a wide energy range, from suprathermal energies up to several hundreds of MeV/nucleon.</p>


2007 ◽  
Vol 52 (5) ◽  
pp. 665-670 ◽  
Author(s):  
YongQiang Hao ◽  
Zuo Xiao ◽  
Hong Zou ◽  
DongHe Zhang

1975 ◽  
Vol 22 (1) ◽  
pp. 575-581 ◽  
Author(s):  
W. P. Aiello ◽  
R. D. Belian ◽  
J. P. Conner ◽  
P. R. Higbie ◽  
W. B. Martin ◽  
...  

2020 ◽  
Author(s):  
Hans Huybrighs ◽  
Christiaan van Buchem ◽  
Aljona Blöcker ◽  
Elias Roussos ◽  
Norbert Krupp ◽  
...  

<p><strong>Introduction</strong></p><p>The flux of energetic ions (protons, oxygen and sulfur) near the Galilean moons were measured by the Energetic Particle Detector (EPD) on the Galileo mission (1995 - 2003). Near Galilean moons (such as Io and Europa) depletions of the energetic ion flux, of several orders of magnitude, were identified.</p><p>Such energetic ion depletions can be caused by the absorption of these particles onto the moon’s surfaces or by the loss due to charge exchange with neutral molecules in the atmospheres or potential plumes. To interpret the depletion features in the EPD data, a Monte Carlo particle tracing simulation has been conducted. The expected fluxes of the energetic ions are simulated under different scenarios including those with and without an atmosphere or plume. By comparing the simulated flux [YF1] to the EPD data, we investigate the cause of the depletion features with particular focuses on Europa and Io flybys.</p><p><strong>Results</strong></p><p>For Europa we report the following findings:</p><ul><li>For flyby E12 we find that a global atmosphere should produce a depletion region along the trajectory that is symmetrical to the closest approach, for energetic protons in the energy range of 80-220 keV. No such feature is visible in the data. Upper limits of the atmosphere are consistent with surface densities (⩽ 10<sup>8 </sup>cm<sup>-3</sup>) and scale heights (50-350 km) of previous studies. We find that a depletion of energetic protons (80-220 keV) occurring before closest approach is consistent with the field perturbations associated with a plume. This plume features coincides in time with the plume reported by Jia et al., 2018.</li> <li>For flyby E26 we find that the depletions of energetic protons (80-220 keV) are consistent with a simulation that takes into account the perturbations of the fields as calculated by an MHD simulation and atmospheric charge exchange. Furthermore, a depletion feature occurring shortly after closest approach is consistent with the field perturbations associated with a plume, located near the plume reported by Arnold et al., 2019.</li> <li>From these investigations, we confirm, independently from previous reports, that the Galileo spacecraft could have passed near plumes.</li> </ul><p>For Io we report the following results:</p><ul><li>We identify regions of proton (80-220 keV) depletions during Io flybys I24, I27 and I31 extending beyond one Io radius. The depletions features are not consistent with Io as an inert body. We investigate atmospheric charge exchange as a cause for the depletions.</li> </ul>


2021 ◽  
Author(s):  
Daniel Pacheco ◽  
Alexander Kollhoff ◽  
Robert F. Wimmer-Schweingruber ◽  
Johan L. Freiherr von Forstner ◽  
Christoph Terasa ◽  
...  

<p>Solar Orbiter was launched in February 2020 carrying the most complete set of in-situ and remote sensing instruments, for the study of the Sun and the heliosphere. The Energetic Particle Detector (EPD) on board of Solar Orbiter was switched on on 28 February 2020 and, since then, it has provided us with measurements of the energetic particles traveling through the inner heliosphere. The EPD suite is composed of a set of different sensors measuring electrons, protons and ions in a wide range of energies.</p><p>The Electron-Proton Telescope (EPT) was designed to measure electrons and ions with energies of 35-4000keV and 45-7000keV respectively. By utilizing the so-called magnet/foil-technique, EPT is capable of measuring energetic particles with a high temporal and energy resolution while obtaining directional information from its four different fields of view. Although EPT is well suited for the study of solar energetic particle events, instrumental effects such as the contamination of EPT data products by GCR particles need to be understood for a correct interpretation of the data.</p><p>We will present our current understanding of the background and calibration of EPT based on the data gathered during the first year of Solar Orbiter’s mission.</p>


2021 ◽  
Author(s):  
Alexander Kollhoff ◽  
Daniel Pacheco ◽  
Robert F. Wimmer-Schweingruber ◽  
Johan von Forstner ◽  
Lars Berger ◽  
...  

<p>Solar Orbiter’s Energetic Particle Detector (EPD) was commissioned in early 2020 and has since been returning data from the inner heliosphere. Despite the low activity in the current deep and extended solar minimum, EPD has observed a number of solar particle events and numerous other enhancements of energetic particles. As one of the four complementary EPD sensors, the Electron-Proton Telescope (EPT) covers the gap between the high and low particle-energy measurements of HET and STEP. With four double-ended telescopes, EPT is capable of measuring electrons and ions in an energy range of 35-400keV and 45-7000keV respectively, while providing anisotropy information from four different viewing directions.</p><p>We will present a first overview of EPT measurements, exhibiting some of the EPT data products which are made available by the European Space Agency (ESA).</p><p>In order to provide the community a deep insight into the data, we will go through different aspects of the measurements, including the current status of the intercalibration with the other EPD instruments.</p>


2013 ◽  
Vol 213 (1-4) ◽  
pp. 289-346 ◽  
Author(s):  
B. H. Mauk ◽  
D. K. Haggerty ◽  
S. E. Jaskulek ◽  
C. E. Schlemm ◽  
L. E. Brown ◽  
...  

2020 ◽  
Author(s):  
Johannes Marquardt ◽  
Bernd Heber ◽  
Robert Elftmann ◽  
Robert Wimmer-Schweingruber

<p>Anomalous cosmic rays (ACRs) are well-suited to probe the transport conditions of energetic particles in the innermost heliosphere. We revisit the HELIOS Experiment 6 (E6) data in view of the upcoming Solar Orbiter Energetic Particle Detector (EPD) suite that will perform measurements during a comparable solar minimum within the same distance.</p><p>Adapting the HELIOS energy ranges for oxygen and carbon to the ones given by the High Energy Telescope (HET) allows us to determine predictions for the upcoming measurements but also to put constraints on particle transport models that provide new insight into the boundary conditions close to the Sun.</p><p>We present here the adapted energy spectra of galactic cosmic ray (GCR) carbon and oxygen, as well as of ACR oxygen during solar quiet time periods between 1975 to 1977. Due to the higher energy threshold of HET in comparison to E6 gradients of about 20% at 15 MeV/nucleon are expected. The largest ACR gradient measured by E6 was obtained to be about 75% between 9 and 13 MeV/nucleon and 0.4 AU and 1 AU.</p>


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