Brötzner, J., Biber, H. A., Jäggi, N., Szabo, P. S., Cupak, C., Galli, A., Wurz, P., & Aumayr, F. (2023, September 11). Erosion of the Lunar Surface by Solar Wind Ions [Conference Presentation]. 24th International Workshop on Inelastic Ion-Surface Collisions (IISC-24), Charleston, South Carolina, United States of America (the).
indicated in fig. 1. To model the exosphere creation, physical quantities such as the sputtering yield
and the angular distribution of sputtered particles must be understood. To achieve this, we have
studied the erosion of two types of samples prepared from lunar soil obtained during the Apollo 16
mission in 1972. The lunar soil material was either pressed into pellets (analogous to the description
in [2]), or used to grow thin films of typically 100 nm thickness onto quartz resonators through
Pulsed Laser Deposition (PLD).
Typical ions found in the solar wind (hydrogen, helium) were used as projectiles with an impact
energy of l keY/amu, equivalent to the medium solar wind velocity of 440 km/s. To measure mass
depletion caused by ion sputtering, thin PLD films were used in a Quartz Crystal Microbalance
(QCM) setup that directly measured changes in the resonance frequency of the QCM. This
methodology was previously tested and refined using Lunar and Mercury analog materials [3, 4].
In the case of pellet samples made from lunar
soil material, an additional QCM was used to
collect sputtered particles. By collecting
sputtered material at different polar angles, the
setup detern1ined the angular distribution of the
emitted particle flux. These measurements
indirectly allowed to access the total sputtering
yield of pellet samples in relation to thin film
samples through differential sputter yield
measurements [5].
Figure 1: lnteraction processes leading to surface erosion
ofairless planetary bodies such as the Moon and release
of refractory and volatile species into the exospbere.
Differences between thin film and pressed pellet samples could be attributed to different surface
roughness. For this purpose, simulations with the codes SPRAY [6] and SDTrimSP-3D [7, 8] were
conducted, which yielded very good agreement. We will present our experimental findings for both
types of samples along with simulation approaches.
References
[1] P. Wurz et al., Space Sei. Rev. 218, 10 (2022)
[2] N. Jäggi et al., 1 Icarus 365, (2021) 114492
[3] P. S. Szabo et al., Astrophys. J. 891, (2020) 100
[4] P. S. Szabo et al., J. Geophys. Res.: Planets 125, (2020) e2020JE006583
[5] H. Biber et al., Planet. Sei. J. 3, (2022) 271
[6] C. Cupak et al., Appl. Surf. Sei. 570, (2021) 151204
[7] U. von Toussaint, Phys. Scr. Tl 70, (2017) 014056
[8] P. S. Szabo et al., Nucl. Jnstr. Meth. B 522, (2022) 47