ARTEMIS: A complete mission architecture to bridge the gap between humanity and near-Earth asteroids

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dc.contributor.author Cano, Jorge
dc.contributor.author Cunill, Jordi
dc.contributor.author Diaz, Albert Josep
dc.contributor.author Golemis, Aris
dc.contributor.author Gupta, Subham
dc.contributor.author Innes, Daniel
dc.contributor.author Maiden, David
dc.contributor.author March, Kieran
dc.contributor.author Rael, Harvey
dc.contributor.author Shawe, James
dc.contributor.author Sierra, Victor
dc.contributor.author Torrents, Alejandro
dc.contributor.author Zorzoli Rossi, Elena
dc.contributor.author Machuca, Pablo
dc.contributor.author Neves, Rita
dc.contributor.author Sanchez Cuartielles, Joan Pau
dc.date.accessioned 2018-11-28T15:54:40Z
dc.date.available 2018-11-28T15:54:40Z
dc.date.issued 2018-10-01
dc.identifier.citation Jorge Cano, Jordi Cunill, Albert Josep Diaz, et al., ARTEMIS: A complete mission architecture to bridge the gap between humanity and near-Earth asteroids. Proceedings of the 69th International Astronautical Congress 2018 (IAC ’18), 1-5 October 2018, Bremen, Germany en_UK
dc.identifier.uri https://www.iac2018.org/
dc.identifier.uri https://iafastro.directory/iac/paper/id/45234/summary/
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/13679
dc.description.abstract Asteroid retrieval missions have recently attracted increasing interest from the community and could provide opportunities for scienti c exploration, resource utilisation and even the development of planetary defence strategies. This paper was developed as a result of a 6-month MSc group project, realised by a total of 14 students at Cran eld University pursuing the Astronautics & Space Engineering degree. An overall system design is proposed for a technology demonstrator mission to move a near-Earth asteroid into an easily-accessible location where it could be further explored by future missions. The target nal orbit is a southern halo orbit around the Lagrange point (L2) on the Sun-Earth system. ARTEMIS (Asteroid Retrieval Technology Mission) abides by ESAs constraints for a Large (L) mission call: realised in only one launch with Ariane 64, an operational duration of less than 15 years and a cost at completion of at most e1100M. The proposed mission combines the design of optimal trajectories, employs advanced solar electric propulsion and introduces a be tting level of spacecraft autonomy. The target is the 2006 RH120 asteroid, with an approximate diameter of 6.5 m and mass of roughly 350 tons. To re ne existing data, the ARROW CubeSat mission (Asteroid Reconnaissance to Research Object Worthiness) is to be launched a year prior to the main mission to probe the asteroid via a y-by. ARROW will provide valuable information, such as the asteroids spin rate, rotational axis and better mass estimate, increasing the overall chance of mission success. The main mission will then capture and secure the asteroid using a mechanism of arm-like booms with xenon- lled VectranTM bags. To allow for proper adaptability to the objects shape and mass distribution, as well as preserve the asteroid unaltered, the mechanism is fully contained in fabric that encapsulates the asteroid. The paper concludes that such a mission is conditionally feasible, and summarises the design process resulting in the nal overall mission baseline design. It also examines the practicality of the suggested design for future missions such as space debris removal or its ability to retrieve celestial bodies with variable mass and shape. Proper adaptation of the design could allow for retrieval of similar size or smaller objects. The future implementation of this mission may further the understanding of the origin of the solar system and act as a catalyst to a new celestial body exploitation industry. en_UK
dc.language.iso en en_UK
dc.publisher International Astronautical Federation en_UK
dc.title ARTEMIS: A complete mission architecture to bridge the gap between humanity and near-Earth asteroids en_UK
dc.type Conference paper en_UK


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