Mr. Venkateswaran Ramaswamy Profile

Venkateswaran Ramaswamy

at Indian Space Research Organisation

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Publications (2)

SPIE Journal Paper | 25 November 2022

Optical metrology on primary mirror of visible emission line coronagraph on board Aditya-L1 mission

Venkata Suresh Narra, Darshika Singh, Natarajan Venkatasubramanian, Vishweshwar Rao Budhiraju, Bhavana Hegde, Nishchith Bhat, Utkarsha Dasamantarao, Pawan Kumar Somasundaram, Venkateswaran Ramaswamy, Umesh Kamath Padavu, Kuppuswamy Venkatesan Sriram, Raghavendra Prasad Budihal

JATIS, Vol. 8, Issue 04, 044004, (November 2022) https://doi.org/10.1117/12.10.1117/1.JATIS.8.4.044004

KEYWORDS: Mirrors, Coronagraphy, Optical metrology, Solar processes, Scatter measurement, Optical spheres, Contamination, Coating, Autoregressive models, Reflectivity

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Proceedings Article | 31 August 2022 Poster + Paper

The thermal filter for the Solar Ultraviolet Imaging Telescope (SUIT) on-board Aditya-L1

Avyarthana Ghosh, Ravi Kesharwani, Aafaque Khan, Sreejith Padinhatteeri, Durgesh Tripathi, A. Ramaprakash, Ketan Patel, Tayaramma D. P. V. Jalluri, G. R. Madhumalathi, R. Venkateshwaran, S. Elumalai, Kinshuk Gupta, J. P. Nair, H. Sparrow, R. S. Worlikar, Anit Gupta, Sanjoy Sen

Proceedings Volume 12181, 121813O (2022) https://doi.org/10.1117/12.2629760

KEYWORDS: Optical filters, Telescopes, Coating, Charge-coupled devices, Ultraviolet telescopes, Reflection, Ultraviolet radiation, Sun, Visible radiation, Space telescopes, Bandpass filters, Gamma radiation

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The solar ultraviolet imaging telescope (SUIT) is an imaging telescope on-board the Aditya-L1 satellite, which is India’s maiden space mission dedicated solely to solar observations. The spatially resolved, high cadence observations are designed to be taken in eleven science filters with full width half maxima ranging between 0.1–58 nm and spread over the near-ultraviolet (NUV) domain of the solar spectrum (200–400 nm). The huge incoming solar flux, limited by the linearity regime performance of the charge coupled device (CCD) as well as the thermal operational constraints, mandate the use of an entrance aperture filter, the thermal filter (TF), for SUIT. The design of this filter is, further, constrained by exposure time and enhanced emission of the sun during eruptive events. From performance perspective, the TF reflects ∼50% of the incident radiation and allows only 0.1–0.45% of the incoming flux to pass within 200–400 nm. The transmission on either side of the operational range is satisfactorily reduced, so as to ensure minimum unwanted light leaking into the imaging system. Therefore, the TF plays a significant role in increasing the photometric efficiency as well as maintaining the operational temperature of the telescope. To the best of our knowledge, this is the first time any attempt of designing and manufacturing any such rejection filter aiming optimized performance in the NUV range is being done for a space-based imaging solar telescope. The choice of materials for substrate and coating for the filter poses several challenges in terms of contamination, corrosion/ oxidation, durability during manufacturing process, long-term exposure to harsh space environment as well as formation of pinholes. The transmission and reflection profiles of the fabricated TF is satisfactory to meet our design and technical constraints. The TF is also qualified for various environmental and radiation conditions. The transmission of the TF is seen to be well within our allowed margins (±10% of the design value) even after being exposed to these qualification tests.

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