Abstract:A comparative study using a fluid-based analytic solution, hybrid particle-ion fluid-electron particle-in-cell (PIC), and fully kinetic PIC is carried out to examine a collisionless, mesothermal plasma flow over a large, unbiased plate. We find that the plasma wake may be characterized into two regions based on the electron characteristics: a fluid electron expansion region and a kinetic electron expansion region. In the fluid electron expansion region, the electrons may be considered to be an equilibrium flui… Show more
“…Hence, the proton flux collected by PSRs surface is that from a plasma wake. As the solar wind plasma expands into the wake, the ion velocity component normal to each expansion characteristic line equals to the ion acoustic speed (Wang & Hastings, 1992; Wang & Hu, 2018). For an order of magnitude estimation, we take the proton density above the lunar surface to be n ∼ 10 cm −3 and the proton impingement velocity to be the ion acoustic velocity km/s.…”
Molecular dynamics simulations are carried out to investigate dielectric breakdown of lunar regolith induced by space weather events and its potential effects on water ice formation on lunar surface. We find that dielectric breakdown can trigger the water formation process by breaking the chemical bonds of regolith grains and exposing the oxygen atoms to react with the hydrogen implanted by solar wind. In the permanently shadowed region, the water molecules formed become attached to regolith grains in the molecular structure of ice after the event. Thus, dielectric breakdown can also enable the preservation of water molecules by changing the hydrophobicity of regolith grains.
“…Hence, the proton flux collected by PSRs surface is that from a plasma wake. As the solar wind plasma expands into the wake, the ion velocity component normal to each expansion characteristic line equals to the ion acoustic speed (Wang & Hastings, 1992; Wang & Hu, 2018). For an order of magnitude estimation, we take the proton density above the lunar surface to be n ∼ 10 cm −3 and the proton impingement velocity to be the ion acoustic velocity km/s.…”
Molecular dynamics simulations are carried out to investigate dielectric breakdown of lunar regolith induced by space weather events and its potential effects on water ice formation on lunar surface. We find that dielectric breakdown can trigger the water formation process by breaking the chemical bonds of regolith grains and exposing the oxygen atoms to react with the hydrogen implanted by solar wind. In the permanently shadowed region, the water molecules formed become attached to regolith grains in the molecular structure of ice after the event. Thus, dielectric breakdown can also enable the preservation of water molecules by changing the hydrophobicity of regolith grains.
“…It is important to note that PSP is in a mesothermal plasma environment with plasma ion thermal velocities lower than the SW (∼300 km/s) and spacecraft speeds (up to 197 km/s), and plasma electron thermal velocities that remain greater than the spacecraft and solar wind velocities. A spacecraft in a mesothermal plasma forms a wake behind it (Ergun et al., 2010; Wang & Hastings, 1992; Wang & Hu, 2018). In addition to negative potential wake, for PSP an electrostatic barrier forms in the front of the spacecraft, as the ambient electrons penetrate the barrier while the photoelectrons and SE cannot (Ergun et al., 2010).…”
Langmuir Probes have been used extensively in space missions to measure the density and plasma potential variations of the environment with respect to the probes (
“…[6][17]). However, the electron dynamics in wake regions have not yet been examined in detail [18]. In this study, we perform threedimensional electrostatic PIC simulations to examine a wake, considering in particular the plasma depletion region in the wake from the viewpoint of electron dynamics.…”
Section: Y Miyake Is With Education Center On Computational Science Andmentioning
We demonstrated the existence of a distorted plasma depletion region in a satellite wake through threedimensional electrostatic particle-in-cell (PIC) plasma simulations. It is commonly known that a wake is formed in the downstream region of a satellite in a magnetized plasma flow. Our simulation shows that the plasma depletion region in the wake is distorted in the plane perpendicular to the static magnetic field. This distortion is asymmetric with respect to the plasma flow direction in the satellite rest frame of reference. We found that the asymmetric structure of the plasma depletion region is caused by non-uniform local drift motion of electrons around the depletion region. By test particle simulations in which electron trajectories are traced in fixed fields obtained in the PIC simulation, we confirmed that cold electrons which have a Larmor radius less than the size of the satellite can cause the asymmetric structure of the plasma depletion in the wake.
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