E-viri
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Trebi-Ollennu, A.; Ali, K. S.; Rankin, A. L.; Tso, K. S.; Assad, C.; Matthews, J. B.; Deen, R. G.; Alexander, D. A.; Toda, R.; Manohara, H.; Mojarradi, M.; Wolf, M.; Wright, J. R.; Jeng Yen; Hartman, F.; Bonitz, R. G.; Sirota, A. R.; Alkalai, L.
2012 IEEE Aerospace Conference, 2012-MarchConference Proceeding
This paper describes a high fidelity mission concept systems testbed at JPL, called Lunar Surface Operations Testbed (LSOT). LSOT provides a unique infrastructure that enables mission concept studies designers to configure and demonstrate end-to-end surface operations using existing JPL mission operations and ground support tools, Lander, robotic arm, stereo cameras, flight software, and soil simulant (regolith), in a high fidelity functional testbed. This paper will describe how LSOT was used to support the MoonRise mission concept study. MoonRise: Lunar South Pole-Aitken Basin Sample Return Mission would place a lander in a broad basin near the moon's South Pole and return approximately two pounds of lunar materials to Earth for study. MoonRise was one of three candidate missions competing to be selected as the third mission for NASA's New Frontiers Program of Solar System Explorations. LSOT was used to demonstrate JPL's extensive experience and understanding of the MoonRise Lander capabilities, design maturity, surface operations systems engineering issues, risks and challenges.
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Leto | Faktor vpliva | Izdaja | Kategorija | Razvrstitev | ||||
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JCR | SNIP | JCR | SNIP | JCR | SNIP | JCR | SNIP |
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Povezave do osebnih bibliografij avtorjev | Povezave do podatkov o raziskovalcih v sistemu SICRIS |
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Vir: Osebne bibliografije
in: SICRIS
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