2015
DOI: 10.1117/12.2190384
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Error budgets for the Exoplanet Starshade (Exo-S) probe-class mission study

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Cited by 15 publications
(19 citation statements)
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“…To reduce reflected glint, the optical edges must achieve razor sharpness, with an edge radius of curvature ≤1 μm. 31 The edges must also maintain a precision shape when deployed, and remain optically dark, with low reflectivity. Machined graphite and chemically etched metal edges are both close to meeting the necessary performance, with the former lacking a small enough edge radius and the latter lacking the deployed shape tolerance.…”
Section: Optical Edgesmentioning
confidence: 99%
“…To reduce reflected glint, the optical edges must achieve razor sharpness, with an edge radius of curvature ≤1 μm. 31 The edges must also maintain a precision shape when deployed, and remain optically dark, with low reflectivity. Machined graphite and chemically etched metal edges are both close to meeting the necessary performance, with the former lacking a small enough edge radius and the latter lacking the deployed shape tolerance.…”
Section: Optical Edgesmentioning
confidence: 99%
“…Even at a distance of tens of thousands of kilometers, solar glint from the metallic, razor-sharp edges is the brightest source of instrument background. 15 For the SRM starshade, roughly 130 m of edge contributes to the glint, of which ∼10 m has a strong specular component that samples the region θ ∼ 0 in Figs. 4 and 8.…”
Section: Modeling Solar Glint Lobesmentioning
confidence: 94%
“…In fact, it is several times larger than any other instrument-related background contributor including stellar diffraction due to starshade shape errors, stellar and solar leakage through micrometeoroid holes in the optical shield, and reflection of the Milky Way and other astrophysical objects from the telescope-facing surface. 15 The SRM's focus on the closest stars, with planets appearing well beyond the IWA, gives ample habitable zone access with minimal interference from the glint lobes. Nonetheless, it is desirable to significantly reduce solar glint to provide the best possible SNR.…”
Section: Mission Performance Assessmentmentioning
confidence: 99%
“…To be a viable starshade occulter, it must fit within the launch vehicle and achieve positioning accuracy of ≤20 cm [60]. The starshade must have low scattering at its edges, so as to not generate stray light problems, creating the requirement that the edge radius of curvature (RoC) should be ≤10 μm [64] and an edge specular reflectivity ≤10%.…”
Section: Uv/optical/ir Sciencementioning
confidence: 99%