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NASA'S Robotic Lunar Lander Development Project
Institution:1. NASA Marshall Space Flight Center, Huntsville AL 35812, United States;2. The Johns Hopkins University Applied Physics Laboratory, Laurel MD 20723, United States;1. College of Engineering and Physical Sciences, University of Guelph, Guelph, ON N1G 2W1, Canada;2. Joint Center for Earth Systems Technology, University of Maryland, Baltimore County, Baltimore, MD 21250, United States;1. Jet Propulsion Laboratory, NASA, 4800 Oak Grove Dr, Pasadena, CA, 91109, USA;2. ispace, inc., 3-1-6, Azabudai, Minato, Tokyo, 106-0041, Japan;3. Institute of Space and Astronautical Science, JAXA, 3-1-1 Yoshinodai, Sagamihara, Kanagawa, 229-8510, Japan;1. Key Laboratory of Space Utilization, Technology and Engineering Center for Space Utilization, Chinese Academy of Sciences, 9 Dengzhuang S Rd., 100094, Beijing, China;2. IMCCE, Observatoire de Paris, Université PSL, CNRS, 77 Av. Denfert-Rochereau, 75014 Paris, France;3. University of Chinese Academy of Sciences, 9 Dengzhuang S Rd., 100094 Beijing, China;1. Institute for Space Technology and Space Applications, Bundeswehr University Munich, Werner-Heisenberg-Weg 39, 85579 Neubiberg, Bavaria, Germany;2. Centre for Organismal Studies,University of Heidelberg, Im Neuenheimer Feld 234, 69120 Heidelberg, Baden-Württemberg, Germany;3. Faculty of Aerospace Engineering, FH Aachen University of Applied Sciences, Hohenstaufenallee 6, 52064 Aachen, Germany;4. Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Oberpfaffenhoffen, Bavaria, Germany;1. JAXA, ISAS, Yoshinoday 3-1-1, Sagamihara, Kanagawa, 155-0031 Japan;2. Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109-8099, USA;1. Department of Physical Sciences, The Open University, Milton Keynes, UK;2. Faculty of Earth and Life Sciences, VU University, Amsterdam, The Netherlands;3. Department of Geology, Northern Arizona University, USA;4. School of Earth, Atmospheric, and Environmental Sciences, University of Manchester, UK;5. Scripps Institute for Oceanography, UC San Diego, USA;6. Cockrell School of Engineering, University of Texas, Austin, USA;7. School of Engineering and Applied Sciences, Columbia University, USA;8. The Boeing Company, Houston, USA;9. Center for Lunar Science and Exploration, Lunar and Planetary Institute, USA
Abstract:Over the last 5 years, NASA has invested in development and risk-reduction activities for a new generation of planetary landers capable of carrying instruments and technology demonstrations to the lunar surface and other airless bodies. The Robotic Lunar Lander Development Project (RLLDP) is jointly implemented by NASA Marshall Space Flight Center (MSFC) and the Johns Hopkins University Applied Physics Laboratory (APL). The RLLDP team has produced mission architecture designs for multiple airless body missions to meet both science and human precursor mission needs. The mission architecture concept studies encompass small, medium, and large landers, with payloads from a few tens of kilograms to over 1000 kg, to the Moon and other airless bodies. To mature these concepts, the project has made significant investments in technology risk reduction in focused subsystems. In addition, many lander technologies and algorithms have been tested and demonstrated in an integrated systems environment using free-flying test articles. These design and testing investments have significantly reduced development risk for airless body landers, thereby reducing overall risk and associated costs for future missions.
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