EPSC Abstracts
Vol. 19, EPSC2026-885, 2026, updated on 02 Jul 2026
https://doi.org/10.5194/epsc2026-885
Europlanet Science Congress 2026
© Author(s) 2026. This work is distributed under
the Creative Commons Attribution 4.0 License.
Oral | Wednesday, 09 Sep, 12:15–12:27 (CEST)| Room Uranus (Swing)
Enceladus surface: modeling intrusion depth for future lander missions
Bastian Gundlach1, Ben Aussel1, Tina Rückriemen-Bez1, Carsten Güttler1, Nils Ligterink2, Stéphanie Cazaux2, Axel Hagermann3, and Jürgen Blum4
Bastian Gundlach et al.
  • 1Universität Münster, Institut für Planetologie, Münster, Germany (bastian.gundlach@uni-muenster.de)
  • 2Faculty of Aerospace Engineering, Delft University of Technology, Delft, The Netherlands
  • 3LTU, 98192 Kiruna, Sweden
  • 4Institute for Geophysics and Extraterrestrial Physics, TU Braunschweig, 38106 Braunschweig, Germany

Enceladus, Saturn’s sixth-largest moon, is encased in a crust of nearly pure water ice that makes it one of the most reflective bodies in the Solar System (Howett et al., 2010). This "fresh-material"-like appearance is due to the continuous fallout of icy grains from the moon’s massive south polar plume (Postberg et al., 2011), which recoats the surface in a bright, porous regolith.

Enceladus is arguably the most geophysically active moon in the Solar System, presenting a high-priority target for the next generation of planetary exploration. Recognizing its immense astrobiological potential, the European Space Agency (ESA) has identified an Enceladus orbiter and lander as the primary candidate for its L4 flagship mission within the Voyage 2050 framework.

Current data suggest a surface dominated by a continuous fallout of plume-derived ice grains, ranging from sub-micron to tens of micrometers in diameter (Jaumann et al., 2008; Postberg et al., 2011; Scipioni et al., 2017; Morello & Berg, 2024). While the moon’s south polar plumes provide a direct window into its subsurface ocean (Postberg et al., 2009), the physical state and observable signatures of the resulting surface regolith remain difficult to directly probe and therefore poorly constrained.

Fortunately, experiments have provided the first insights into the compressional behavior (compression curve: Φ(p); here Φ is the volume filling factor and p the applied pressure) of micrometer-sized water ice particles at low temperatures (Lorek et al., 2016; Kreuzig et al., 2023), which can be translated into a lander intrusion depth. Based on the recent work by Blum et al. (2026), the laboratory findings and the very low gravity of the icy moon, we developed a model to predict the intrusion depth of a potential lander. Initial results indicate intrusion depths in the mm to cm range as presented in Fig. 1, while further details regarding the model will be presented at the conference.

 

Fig. 1: Monte Carlo analysis showing a nominal intrusion depth of 0.4 cm (analytical mean), and 1.9 cm (numerical iterative mean).

 

References:

Howett et al. (2010) – DOI: 10.1016/j.icarus.2009.07.016

Postberg et al. (2011) – DOI: 10.1038/nature10175

Jaumann et al. (2008) – DOI: 10.1016/j.icarus.2007.09.013

Scipioni et al. (2017) – DOI: 10.1016/j.icarus.2017.02.012

Brown et al. (2006) – DOI: 10.1126/science.1121031

Gundlach et al. (2018) – DOI: 10.1093/mnras/sty1839

Morello & Berg (2024) – DOI: 10.1016/j.jqsrt.2024.109018

Lorek et al. (2016) – DOI: 10.1051/0004-6361/201526565

Kreuzig et al. (2023) – DOI: 10.1093/rasti/rzad049

Blum et al. (2026) – DOI: 10.1051/0004-6361/202558471

How to cite: Gundlach, B., Aussel, B., Rückriemen-Bez, T., Güttler, C., Ligterink, N., Cazaux, S., Hagermann, A., and Blum, J.: Enceladus surface: modeling intrusion depth for future lander missions, Europlanet Science Congress 2026, The Hague, The Netherlands, 7–11 Sep 2026, EPSC2026-885, https://doi.org/10.5194/epsc2026-885, 2026.