Response of Mars O+ pickup ions to the 8 March 2015 ICME: Inferences from MAVEN data‐based models. Issue 21 (5th November 2015)

• Record Type: Journal Article
• Authors: Curry, S. M.; Luhmann, J. G.; Ma, Y. J.; Dong, C. F.; Brain, D.; Leblanc, F.; Modolo, R.; Dong, Y.; McFadden, J.; Halekas, J.; Connerney, J.; Espley, J.; Hara, T.; Harada, Y.; Lee, C.; Fang, X.; Jakosky, B.
• Is Part Of: Geophysical research letters. Volume 42:Issue 21(2015:Nov.)
• Page Start: 9095
• Page End: 9102
• Publication Date: 2015-11-05
• Subjects: Mars -- ICME -- pickup ions -- escape -- precipitation; Geophysics -- Periodicals; Planets -- Periodicals; Lunar geology -- Periodicals; 550
• DOI: 10.1002/2015GL065304
• Languages: English
• ISSNs: 0094-8276

Abstract

Abstract: We simulate and compare three phases of the Mars‐solar wind interaction with the 8 March interplanetary coronal mass ejection (ICME) event using Mars Atmosphere and Volatile EvolutioN (MAVEN) mission observations in order to derive heavy ion precipitation and escape rates. The MAVEN observations provide the initial conditions for three steady state MHD model cases, which reproduce the observed features in the solar wind density, velocity, and magnetic field seen along the MAVEN orbit. Applying the MHD results to a kinetic test particle model, we simulate global precipitation and escape maps of O + during the (1) pre‐ICME phase, (2) sheath phase, and (3) ejecta phase. We find that the Case 1 had the lowest precipitation and escape rates of 9.5 × 10 25 and 4.1 × 10 25 s −1, Case 2 had the highest rates of 9.5 × 10 25 and 4.1 × 10 25 s −1, and Case 3 had rates of 3.2 × 10 25 and 1.3 × 10 25 s −1, respectively. Additionally, Case 2 produced a high‐energy escaping plume >10 keV, which mirrored corresponding STATIC observations. Key Points: The shock phase of an ICME drives the most ion escape at Mars The shock phase of an ICME has an O + escape rate of 4.1e25/s O sputtering from the shock phase of an ICME may be on the order of 1e26/s