Please use this identifier to cite or link to this item: http://hdl.handle.net/2248/8406
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dc.contributor.authorMishra, Shalabh-
dc.contributor.authorSasikumar Raja, K-
dc.contributor.authorSanal Krishnan, V. U-
dc.contributor.authorVenkata Suresh, Narra-
dc.contributor.authorHegde, Bhavana-
dc.contributor.authorUtkarsha, D-
dc.contributor.authorPriyal, M-
dc.contributor.authorPawan, Kumar-
dc.contributor.authorNatarajan, V-
dc.contributor.authorPrasad, B. R-
dc.contributor.authorSingh, J-
dc.contributor.authorKamath, P. U-
dc.contributor.authorKathiravan, S-
dc.contributor.authorVishnu, T-
dc.contributor.authorSuresha-
dc.contributor.authorSavarimuthu, P-
dc.contributor.authorDesai, Jalshri H-
dc.contributor.authorKumaran, Rajiv-
dc.contributor.authorSagar, Shiv-
dc.contributor.authorKumar, Sumit-
dc.contributor.authorBamrah, Inderjeet Singh-
dc.contributor.authorAmit Kumar-
dc.date.accessioned2024-04-24T06:28:57Z-
dc.date.available2024-04-24T06:28:57Z-
dc.date.issued2024-04-
dc.identifier.citationExperimental Astronomy, Vol. 57, No. 2, 7en_US
dc.identifier.issn0922-6435-
dc.identifier.urihttp://hdl.handle.net/2248/8406-
dc.descriptionRestricted Accessen_US
dc.descriptionThe original publication is available at the springerlink.com-
dc.description.abstractAditya-L1 is the first Indian space mission to explore the Sun and solar atmosphere with seven multi-wavelength payloads, with Visible Emission Line Coronagraph (VELC) being the prime payload. It is an internally occulted coronagraph with four channels to image the Sun at 5000 Å in the field of view 1.05 - 3 R, and to pursue spectroscopy at 5303 Å, 7892 Å and 10747 Å channels in the FOV (1.05 - 1.5 R). In addition, spectropolarimetry is planned at 10747 Å channel. Therefore, VELC has three sCMOS detectors and one InGaAs detector. In this article, we aim to describe the technical details and specifications of the detectors achieved by way of thermo-vacuum calibration at the CREST campus of the Indian Institute of Astrophysics, Bangalore, India. Furthermore, we report the estimated conversion gain, full-well capacity, and readout noise at different temperatures. Based on the numbers, it is thus concluded that it is essential to operate the sCMOS detectors and InGaAs detector at −5◦ and −17◦ C, respectively, at the spacecraft level.en_US
dc.language.isoenen_US
dc.publisherSpringer Natureen_US
dc.relation.urihttps://doi.org/10.1007/s10686-024-09922-2-
dc.rights© The Author(s), under exclusive licence to Springer Nature B.V. 2024-
dc.subjectAditya-L1en_US
dc.subjectVELCen_US
dc.subjectsCMOS detectorsen_US
dc.subjectInGaAs detectorsen_US
dc.titleCalibration of VELC detectors on-board Aditya-L1 missionen_US
dc.typeArticleen_US
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