dc.contributor.author |
Mishra, Shalabh |
|
dc.contributor.author |
Sasikumar Raja, K |
|
dc.contributor.author |
Sanal Krishnan, V. U |
|
dc.contributor.author |
Venkata Suresh, Narra |
|
dc.contributor.author |
Hegde, Bhavana |
|
dc.contributor.author |
Utkarsha, D |
|
dc.contributor.author |
Priyal, M |
|
dc.contributor.author |
Pawan, Kumar |
|
dc.contributor.author |
Natarajan, V |
|
dc.contributor.author |
Prasad, B. R |
|
dc.contributor.author |
Singh, J |
|
dc.contributor.author |
Kamath, P. U |
|
dc.contributor.author |
Kathiravan, S |
|
dc.contributor.author |
Vishnu, T |
|
dc.contributor.author |
Suresha |
|
dc.contributor.author |
Savarimuthu, P |
|
dc.contributor.author |
Desai, Jalshri H |
|
dc.contributor.author |
Kumaran, Rajiv |
|
dc.contributor.author |
Sagar, Shiv |
|
dc.contributor.author |
Kumar, Sumit |
|
dc.contributor.author |
Bamrah, Inderjeet Singh |
|
dc.contributor.author |
Amit Kumar |
|
dc.date.accessioned |
2024-04-24T06:28:57Z |
|
dc.date.available |
2024-04-24T06:28:57Z |
|
dc.date.issued |
2024-04 |
|
dc.identifier.citation |
Experimental Astronomy, Vol. 57, No. 2, 7 |
en_US |
dc.identifier.issn |
0922-6435 |
|
dc.identifier.uri |
http://hdl.handle.net/2248/8406 |
|
dc.description |
Restricted Access |
en_US |
dc.description |
The original publication is available at the springerlink.com |
|
dc.description.abstract |
Aditya-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.iso |
en |
en_US |
dc.publisher |
Springer Nature |
en_US |
dc.relation.uri |
https://doi.org/10.1007/s10686-024-09922-2 |
|
dc.rights |
© The Author(s), under exclusive licence to Springer Nature B.V. 2024 |
|
dc.subject |
Aditya-L1 |
en_US |
dc.subject |
VELC |
en_US |
dc.subject |
sCMOS detectors |
en_US |
dc.subject |
InGaAs detectors |
en_US |
dc.title |
Calibration of VELC detectors on-board Aditya-L1 mission |
en_US |
dc.type |
Article |
en_US |