A multiple-rendezvous, sample-return mission to two near-Earth asteroids

• Published in: Advances in space research 2011-07, Vol.48 (1), p.120-132
• Main Authors: Duffard, R., Kumar, K., Pirrotta, S., Salatti, M., Kubínyi, M., Derz, U., Armytage, R.M.G., Arloth, S., Donati, L., Duricic, A., Flahaut, J., Hempel, S., Pollinger, A., Poulsen, S.
• Format: Article
• Language: English
• Subjects: Asteroid sample-return mission; Astronomy; Earth Sciences; Earth, ocean, space; Exact sciences and technology; External geophysics; Sciences of the Universe; Solar System exploration; Ultrasonic drilling; Unmanned mission
• ISSN: 0273-1177; 1879-1948
• DOI: 10.1016/j.asr.2011.02.013

We propose a dual-rendezvous mission, targeting near-Earth asteroids, including sample-return. The mission, Asteroid Sampling Mission (ASM), consists of two parts: (i) flyby and remote sensing of a Q-type asteroid, and (ii) sampling of a V-type asteroid. The targeted undifferentiated Q-type are found mainly in the near-Earth space, and to this date have not been the target of a space mission. We have chosen, for our sampling target, an asteroid from the basaltic class (V-type), as asteroids in this class exhibit spectral signatures that resemble those of the well-studied Howardite–Eucrite–Diogenite (HED) meteorite suite. With this mission, we expect to answer specific questions about the links between differentiated meteorites and asteroids, as well as gain further insight into the broader issues of early Solar System (SS) evolution and the formation of terrestrial planets. To achieve the mission, we designed a spacecraft with a dry mass of less than 3 tonnes that uses electric propulsion with a solar-electric power supply of 15 kW at 1 Astronomical Unit (AU). The mission includes a series of remote sensing instruments, envisages landing of the whole spacecraft on the sampling target, and employs an innovative sampling mechanism. Launch is foreseen to occur in 2018, as the designed timetable, and the mission would last about 10 years, bringing back a 150 g subsurface sample within a small re-entry capsule. This paper is a work presented at the 2008 Summer School Alpbach,“Sample return from the Moon, asteroids and comets” organized by the Aeronautics and Space Agency of the Austrian Research Promotion Agency. It is co-sponsored by ESA and the national space authorities of its Member and Co-operating States, with the support of the International Space Science Institute and Austrospace.