Topical issue on EChO - the Exoplanet Characterisation Observatory
Topical issue on EChO - the Exoplanet Characterisation Observatory
复制标题
关于 EChO 的热门问题 - 系外行星特征观测站
DOI:
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发表时间:
2015
期刊:
影响因子:
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通讯作者:
P. Drossart
中科院分区:
文献类型:
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作者:
G. Tinetti;P. Drossart
The concept of a mission devoted to atmospheric characterization of planets through transit spectroscopy was first considered in Europe in 2007, shortly after the DARWIN proposal submitted to the European Space Agency for the first Cosmic Vision call for L-class missions was rejected because of scientific and technical immaturity. Following the decision, both ESA (EP-RAT panel – report in October 2010) and the Exoplanetary Community (Blue Dot Team – Barcelona conference in September 2009) started a discussion to define a scientific and technological roadmap for exoplanetary research. Both groups concluded that an intermediate step was needed, both scientifically and technically, before the characterisation of Earth-like planets could be tackled, and recom-mended a transit spectroscopy mission as a first step to atmospheric characterization. EChO, the Exoplanet Characterisation Observatory, was proposed as a medium class mission candidate in 2010 by a consortium of institutes and universities from ESA member states, in response to the second call for medium class missions in the Cosmic Vision 2015 – 2025 programme. The mission was one of four selected in February 2011 for further study in a Phase 0/A assessment study (Tinetti et al., 2012, Experimental Astronomy , 34, 311 – 353). Soon after, an ESA study team, and a Science Study team comprising scientists from the proposing team and beyond, were assembled. An internal ESA pre-assessment study of EChO was undertaken in the Concurrent Design Facility at ESTEC that provided a baseline mission concept for subsequent study. The industrial and scientific payload studies started in early 2012 and concluded in September, 2013. The industrial studies performed by Astrium (Toulouse) and TAS-F (Cannes) included a review of the mission requirements, the technical design and a programmatic analysis of the mission. The study of the scientific payload – including science ground segment elements and an end-to-end performance simulation