2018
DOI: 10.1038/s41550-018-0549-2
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The Habitable Exoplanet Observatory

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Cited by 43 publications
(46 citation statements)
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“…Dressing et al (2019) found, in the case of an extremely precise and complete RV survey down to 8 cm/s, that the ini-tial search more time of a direct imaging mission would be reduced by 44%. This initial search is predicted to 71% or 48% of the LUVOIR-A or HabEx mission lifetimes respectively (Roberge & Moustakas 2018;Gaudi et al 2018). Thus a significant reduction in the initial search would greatly boost mission scientific yields by allowing for a focus on planet characterization.…”
Section: Nominalmentioning
confidence: 99%
“…Dressing et al (2019) found, in the case of an extremely precise and complete RV survey down to 8 cm/s, that the ini-tial search more time of a direct imaging mission would be reduced by 44%. This initial search is predicted to 71% or 48% of the LUVOIR-A or HabEx mission lifetimes respectively (Roberge & Moustakas 2018;Gaudi et al 2018). Thus a significant reduction in the initial search would greatly boost mission scientific yields by allowing for a focus on planet characterization.…”
Section: Nominalmentioning
confidence: 99%
“…The statistical finding that rocky, temperate exoplanets are common (Dressing & Charbonneau 2015) has received dramatic validation with the discovery of nearby potentially habitable worlds like LHS-1140b, TRAPPIST-1e, TOI-700d, and Kepler-442b (Torres et al 2015;Dittmann et al 2017;Gillon et al 2017;Gilbert et al 2020). Upcoming facilities such as the James Webb Space Telescope, the Extremely Large Telescopes, and the HabEx and LUVOIR mission concepts will have the ability to detect the atmospheres of such worlds and possibly characterize their atmospheric compositions (Rodler & López-Morales 2014;Fujii et al 2018;Lustig-Yaeger et al 2019;LUVOIR Team 2019;Meixner et al 2019;Gaudi et al 2020).…”
Section: Introductionmentioning
confidence: 99%
“…The KPPs and environments derived by S5 for SRM also apply for the Habitable Exoplanet Observatory (HabEx) mission. 11 The main difference between the two missions that impacts the technology development is in the size of the starshade, with the HabEx starshade being twice as large as the SRM starshade. Thus, a full-scale test article for SRM will be only half-scale for HabEx and therefore of lower fidelity.…”
Section: Technology Gaps To Starshade Missionsmentioning
confidence: 99%