| Autor: |
de Castro, Ana I. Gomez, Beitia-Antero, Leire, Miravet-Fuster, Carlos E., Tarabini, Lorenzo, Tomas, Albert, Vallejo, Juan Carlos, Canet, Ada, Sachkov, Mikhail, Kameda, Shingo |
| Rok vydání: |
2019 |
| Předmět: |
|
| Zdroj: |
J. Astron. Telesc. Instrum. Syst. 5(4), 044004 (2019) |
| Druh dokumentu: |
Working Paper |
| DOI: |
10.1117/1.JATIS.5.4.044004 |
| Popis: |
There is a growing interest in Lunar exploration fed by the perception that the Moon can be made accessible to low-cost missions in the next decade. The on-going projects to set a communications relay in Lunar orbit and a deep space Gateway, as well as the spreading of commercial-of-the shelf (COTS) technology for small space platforms such as the cubesats contribute to this perception. Small, cubesat size satellites orbiting the Moon offer ample opportunities to study the Moon and enjoy an advantage point to monitor the Solar System and the large scale interaction between the Earth and the solar wind. In this article, we describe the technical characteristics of a 12U cubesat to be set in polar Lunar orbit for this purpose and the science behind it. The mission is named EarthASAP (Earth AS An exoPlanet) and was submitted to the Lunar Cubesats for Exploration (LUCE) call in 2016. EarthASAP was designed to monitor hydrated rock reservoirs in the Lunar poles and to study the interaction between the large Earth's exosphere and the solar wind in preparation for future exoplanetary missions. |
| Databáze: |
arXiv |
| Externí odkaz: |
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