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50th Lunar and Conference 2019 (LPI Contrib. No. 2132) 1327.pdf

HERACLES: An ESA-JAXA-CSA Joint Study on Returning to the . H. Hiesinger1, M. Landgraf2, W. Carey2, Y. Karouji3, T. Haltigin4, G. Osinski5, U. Mall6, K. Hashizume7, HERACLES Science Working Group, HERACLES International Science Definition Team; 1Institut für Planetologie, Westfälische Wil- helms-Universität, Wilhelm-Klemm-Str. 10, 48149 Münster, Germany ([email protected]), 2European Space Agency (ESA), Directorate of Human and Robotic Exploration Programmes, 3Japan Exploration Agency (JAXA), System Technology Unit, 4Canadian Space Agency (CSA), 5University of Western , Centre for Planetary Science and Exploration, 6Max- Institut für Sonnensystemforschung, 7Ibaraki University, Dept. of Earth Science.

Introduction: In the past two decades, the Mission Concept: The key objectives of Moon has been attracting the growing interest of HERACLES include: (1) Preparing for human space-faring nations for both scientific and ex- lunar missions by implementing, demonstrating, ploration goals, resulting in missions such as and certifying technology elements for human Chandrayaan, SELENE, the Lunar Reconnais- lunar landing, surface operations, and return; (2) sance Orbiter, and GRAIL. Many fundamental Create opportunities for science, particularly concepts of planet formation and evolution, as sample return; (3) Gain scientific and exploration well as Solar System bombardment history, knowledge, particularly on potential resources; have been developed on the basis of lunar sam- and (4) Create opportunities to demonstrate and ples and remote sensing information. Although test technologies and operational procedures for they have been applied to other planetary bod- future Mars missions. To achieve these objec- ies, we are far from completely understanding tives, proposed HERACLES concept will consist these concepts. This necessitates returning to of the Lunar Descent Element (LDE), which will the Moon for extended periods of time with or- be provided by JAXA, the ESA-built Interface biters, landers, rovers, and human explorers. Element that will house the Canadian rover, and Several space agencies have recognized [1] the the European Lunar Ascent Element (LAE) that scientific (and strategic) benefits of returning to will return the samples to the the Moon and the opportunities the Moon offers (Fig. 1). A more detailed description of the engi- for testing hardware and operational procedures neering aspects of the mission is available in an for the exploration and utilization of space be- accompanying paper by the HERACLES Archi- yond Low Earth (LEO). For example, China tecture Working Group [2]. as well as have developed programmatic frameworks of several comprehensive lunar missions within the next 10-20 years, ultimately resulting in putting humans back on the Moon. In this context, the Human Enhanced Robotic Ar- chitecture Capability for Lunar Exploration and Science (HEREACLES) is an ESA-led interna- tional effort to prepare for the return of human missions to the Moon and to provide opportuni- ties for unprecedented science utilizing the lunar Gateway. Currently, HERACLES is a joint

phase-A study of the Fig. 1: The elements of the HERACLES mission. (ESA), the Japan Aerospace Exploration Agency (JAXA), and the (CSA) The 330 kg rover will be deployed from the with NASA and having observer Interface Element via two ramps and will be status. HERACLES will land on the lunar sur- powered by a radioisotope power system that face, demonstrate surface operations, and will will enable the rover to drive more than 100 km return about 15 kg of samples from the surface and to survive lunar night. During particularly to the lunar Gateway to eventually be brought to difficult operations, the rover will be operated Earth by the on board the NASA Ori- from astronauts on the lunar Gateway while it on . Hence, it is intended as a robotic will be operated for of the time from Earth pathway toward sustainable international human (Fig. 2). The current plan foresees that the rover will immediately collect a contingency sample and beyond. upon landing. It will then collect samples along a 50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 1327.pdf

~35 km long traverse from about ten individual provide geochemical/mineralogical information sampling stations and will return them to the along the traverse. The iSDT is evaluating a LAE. The rover will be equipped with a suite of suite of potential landing sites, guided by the scientific instruments (expected combined pay- recommendations of the 2007 NRC report [3] load mass of 90 kg) that will allow us to compre- and several subsequently published documents hensively study the sampling locations and the [e.g., 4]. The list of potential landing sites in- context of the samples, as well as the geology cludes the Schrödinger basin, the Moscoviense along the traverse. The international Science basin, Copernicus crater, Jackson crater, and Definition Team (iSDT) is currently discussing an some young basalts in the Flamsteed region [5]. appropriate instrument suite, which will most The Schrödinger basin has been extensively likely include cameras, spectrometers, a laser studied [e.g., 6-8] and currently serves as a case reflector, and potentially some geophysical in- study to develop mission scenarios and scientific struments. After the samples have been depos- rationales. With a landing in the Schrödinger ited into the LAE, the surface mobility demon- basin, HERACLES could be the first mission to stration phase will begin during which the rover sample farside material, including potentially will go on a >100 km long traverse with the in- South Pole-Aitken material, to sample a basin struments continuously collecting data while melt sheet and deep-seated crustal lithologies, roving. For example, a Ground Penetrating Ra- and to evaluate the In Situ Resource Utilization dar (GPR) could provide an unprecedented view (ISRU) potential (also see our companion ab- into the regolith structure of various terrains vis- stract by [5]). Thus, HERACLES will bridge the ited by the rover. Similarly, a camera permanent- gaps between science, exploration and human ly looking at the wheels of the rover could pro- space flight, and will allow us to accomplish vide us with information on the physical charac- many necessary steps in each of those do- teristics of the regolith while spectrometers could mains.

Fig. 2: The HERACLES mission concept.

References: [1] ISECG (2018), Global Exploration Roadmap; [2] Landgraf et al., (2019), LPSC 50th, this volume; [3] National Research Council (2007), The Scientific Context for Exploration of the Moon: Final Report, ISBN: 0-309-10920-5, 120 pages; [4] Kring and Durda (eds.) (2012), A Global Lunar Landing Site Study to Provide the Scientific Context for Exploration of the Moon, LPI Contribution No. 1694, 688 p. [5] Karouji et al. (2019), LPSC 50th, this volume; [6] Kramer et al. (2013), Icarus 223, 131-148; [7] Potts et al. (2015), Adv. Space Res. 55, 1241-1254 [8] Steenstra et al. (2016), Adv. Space Res. 58, 1050-1065.