, pages 1–12, March 2019. \n
\n
@inproceedings{badescu_sampling_2019,\n\ttitle = {Sampling {Tool} {Concepts} for {Enceladus} {Lander} {In}-{Situ} {Analysis}},\n\tdoi = {10.1109/AERO.2019.8741568},\n\tabstract = {A potential future in-situ lander mission to the surface of Enceladus could be the lowest cost mission to determine if life exists beyond Earth since material from the subsurface ocean, where the presence of hydrothermal activity has been strongly suggested by the Cassini mission, is available on its surface after being ejected by plumes and then settling on the surface. In addition, the low radiation environment of Enceladus would not significantly alter the chemical makeup of samples recently deposited on the surface. A study was conducted to explore various sampling devices that could be used by an in-situ lander mission to provide 1cc to 5cc volume samples to instruments. In addition to temperature and vacuum environmental conditions, the low surface gravity of Enceladus (1\\% of Earth gravity)represents a new challenge for surface sampling that is not met by sampling systems developed for microgravity (e.g., comets and asteroids)or higher gravity (e.g., Europa 13\\%g, Moon 16\\%g, or Mars 38\\%g)environments. It is desired to acquire surface plume material that has accumulated in the top 1cm to ensure acquisition of the least processed material. Several sampling devices were developed or adapted and then tested in simulated conditions that resemble the Enceladus surface properties. These devices and test results are presented in this paper.},\n\tbooktitle = {2019 {IEEE} {Aerospace} {Conference}},\n\tauthor = {Badescu, Mircea and Riccobono, Dario and Ubellacker, Samuel and Backes, Paul and Dotson, Matthew and Molaro, Jamie and Moreland, Scott and Csomay-Shanklin, Noel and Choukroun, Mathieu and Brinkman, Alexander and Genta, Giancarlo},\n\tmonth = mar,\n\tyear = {2019},\n\tnote = {ISSN: 1095-323X},\n\tkeywords = {5cc volume samples, Cassini mission, Earth gravity, Enceladus lander, Enceladus surface properties, Gravity, In, Mars, Ocean temperature, Propulsion, Saturn, Sea surface, Surface treatment, Tools, asteroids, higher gravity, hydrothermal activity, low radiation environment, low surface gravity, lowest cost mission, planetary atmospheres, planetary satellites, planetary surfaces, potential future in-situ lander mission, processed material, sampling devices, sampling systems, sampling tool, seafloor phenomena, size 1.0 cm, space vehicles, subsurface ocean, surface plume material, surface sampling, temperature, vacuum environmental conditions},\n\tpages = {1--12},\n}\n
\n
\n A potential future in-situ lander mission to the surface of Enceladus could be the lowest cost mission to determine if life exists beyond Earth since material from the subsurface ocean, where the presence of hydrothermal activity has been strongly suggested by the Cassini mission, is available on its surface after being ejected by plumes and then settling on the surface. In addition, the low radiation environment of Enceladus would not significantly alter the chemical makeup of samples recently deposited on the surface. A study was conducted to explore various sampling devices that could be used by an in-situ lander mission to provide 1cc to 5cc volume samples to instruments. In addition to temperature and vacuum environmental conditions, the low surface gravity of Enceladus (1% of Earth gravity)represents a new challenge for surface sampling that is not met by sampling systems developed for microgravity (e.g., comets and asteroids)or higher gravity (e.g., Europa 13%g, Moon 16%g, or Mars 38%g)environments. It is desired to acquire surface plume material that has accumulated in the top 1cm to ensure acquisition of the least processed material. Several sampling devices were developed or adapted and then tested in simulated conditions that resemble the Enceladus surface properties. These devices and test results are presented in this paper.\n