Europlanet Science Congress 2022
Palacio de Congresos de Granada, Spain
18 – 23 September 2022
Europlanet Science Congress 2022
Palacio de Congresos de Granada, Spain
18 September – 23 September 2022
EPSC Abstracts
Vol. 16, EPSC2022-985, 2022
https://doi.org/10.5194/epsc2022-985
Europlanet Science Congress 2022
© Author(s) 2022. This work is distributed under
the Creative Commons Attribution 4.0 License.

A Dynamic Model for the Lunar Ejecta Dust Cloud

Maximilian Sommer1, Yanwei Li1, Ralf Srama1, Peter Strub2, Jianqun Yang3, and Xingji Li3
Maximilian Sommer et al.
  • 1University of Stuttgart, Institute of Space Systems, Stuttgart, Germany (sommer@irs.uni-stuttgart.de)
  • 2Max Planck Institute for Solar System Research, Göttingen, Germany
  • 3Harbin Institute of Technology, Harbin, China

The return to the Moon pushed forward by space agencies as well as private companies around the world, has rekindled interest in the Lunar dust environment, which was identified as a major factor in spacecraft safety and reliability considerations during the Apollo missions. Orbiting the Moon from 2013 to 2014, the Lunar Atmosphere and Dust Environment Explorer (LADEE) gathered conclusive evidence for the existence of a permanent, asymmetric dust cloud around the Moon [1]. Micron-sized ejecta particles generated at impact of interplanetary meteoroids on the Lunar surface act as the main source of this high-altitude dust exosphere, which shows a variable density in dependence of annual meteoroid showers.

Here we report on the development of a dynamic model for the lunar ejecta dust cloud. This model simulates cloud particles in a Monte-Carlo fashion, drawing on a combination of existing engineering models and results from hypervelocity impact experiments as model inputs: To emulate the influx of meteoroids we use the Interplanetary Meteoroid Environment Model 2 (IMEM2) [2], developed under ESA contract, as well as a comet stream model based on meteor shower zenith-hourly-rates [3, 4]. To determine angular, velocity, and size distributions of ejecta particles, we resort to three different methods: (1) We use the software Ansys Autodyn to numerically model ejecta particles generated at hypervelocity impacts. (2) Impact experiments with a light-gas gun have been conducted at the Harbin Institute of Technology, to derive ejecta distributions generated by bigger projectiles. (3) We intend to conduct hypervelocity impact experiments with lunar soil simulant at the electrostatic dust-accelerator facility at the University of Stuttgart. The novel experiment set-up, which uses a delay-line-detector to measure micron-sized ejecta particles has recently been verified [5]. Ultimately, the simulated dust ejecta cloud will be fitted to LADEE/LDEX data. This poster-presentation gives an overview of the project and its various modules.

References:
[1] Horányi, M., et al. "A permanent, asymmetric dust cloud around the Moon." Nature 522.7556 (2015): 324-326.
[2] Soja, R. H., et al. "IMEM2: a meteoroid environment model for the inner solar system." Astronomy & Astrophysics 628 (2019): A109.
[3] Jenniskens, Peter. "Meteor stream activity I. The annual streams." Astronomy and Astrophysics 287 (1994): 990-1013.
[4] McBride, Neil. "The importance of the annual meteoroid streams to spacecraft and their detectors." Advances in Space Research 20.8 (1997): 1513-1516.
[5] Li, Yanwei, et al. "Measurement of fragments generated by hypervelocity impacts of micron-sized iron particles at grazing incidents." Advances in Space Research 69.6 (2022): 2629-2635.

How to cite: Sommer, M., Li, Y., Srama, R., Strub, P., Yang, J., and Li, X.: A Dynamic Model for the Lunar Ejecta Dust Cloud, Europlanet Science Congress 2022, Granada, Spain, 18–23 Sep 2022, EPSC2022-985, https://doi.org/10.5194/epsc2022-985, 2022.

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