Deimos In-Situ science: the TASTE CubeSat lander regolith sampling subsystem
- Paper number
IAC-24,A3,4B,10,x87961
- Author
Ms. Alice Dottori, Politecnico di Milano, Italy
- Coauthor
Mr. Francesco De Cecio, Politecnico di Milano, Italy
- Coauthor
Mr. Enrico Belloni, Politecnico di Milano, Italy
- Coauthor
Dr. Giovanni Zanotti, Politecnico di Milano, Italy
- Coauthor
Prof. Michèle Lavagna, Politecnico di Milano, Italy
- Coauthor
Dr. John Robert Brucato, INAF - Astrophysical Observatory of Arcetri, Italy
- Coauthor
Dr. Fabrizio Fiore, INAF - Istituto Nazionale di AstroFisica, Italy
- Coauthor
Dr. Alberto Fedele, ASI - Italian Space Agency, Italy
- Coauthor
Dr. Marilena Amoroso, Italian Space Agency (ASI), Italy
- Coauthor
Dr. Andrea Meneghin, Italy
- Year
2024
- Abstract
The sampling and analysis of the Deimos surface regolith would allow to better understand the formation and evolution of the Martian system. The TASTE CubeSat mission, funded by the Italian Space Agency in the framework of the Alcor program, would be the first to attempt this challenge. However, the mission faces the constraint of a limited 1U volume available for the regolith sampling subsystem. To address this issue, a miniaturized drilling system is developed to collect, store, and select samples for analysis. The system is designed to target depths in the order of centimetres. The sampling unit has an external helicoil that ensures efficient soil penetration. Additionally, an internal helicoil is included to convey the regolith to the collection and storing chamber. Organic compounds are here extracted from the regolith and then moved through fluidic equipment to the Lab-on-Chip analysis subsystem, developed by the Italian National Institute for Astrophysics (INAF). The collection chamber is designed to store the whole sample while ensuring its sealing during fluidic operations. Adapting to the limitations of a 4U CubeSat, the drill design and operations prioritize minimizing the counter-reaction of the soil on the lander, thus reducing the anchoring requirements. The design of the drill itself shall be able to face different conditions once on the Deimos surface, given the uncertainties on the mechanical and physical properties of the soil. A preliminary model of the drilling unit is currently being developed to account for a wide range of uncertainties. The purpose is to address the challenges of the mission and estimate the forces that will be exchanged between the sampling system, the lander, and the terrain, thereby informing the need for a potential anchoring system for the CubeSat lander. Additionally, preliminary simulations are conducted to evaluate the performance of the internal helicoil in conveying regolith. State-of-the-art drilling systems have demonstrated their capabilities in space missions of classical sizes. However, adapting them to meet the CubeSat standards requires extensive re-engineering due to the strict limitations on size, power, and mass. This presents an exciting opportunity to develop innovative solutions that can support planetary exploration using CubeSats as a framework.
- Abstract document
- Manuscript document
IAC-24,A3,4B,10,x87961.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.