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Tessy Thomas

Indian scientist From Wikipedia, the free encyclopedia

Tessy Thomas
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Tessy Thomas (born April 1963) is an Indian aerospace engineer and former Director General of Aeronautical Systems and the former Project Director for Agni-IV ballistic missile in Defence Research and Development Organisation.[1]

Quick Facts Director General (Aeronautical Systems), DRDO, Preceded by ...
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Early life

Tessy Thomas was born during April 1963 in Kerala's Alappuzha.[citation needed]

Career

She joined the Defence Research and Development Organisation (DRDO) in 1988.[citation needed] Thomas began in her career working upon the Agni missile series, where she initially contributed to the guidance and control systems, focusing specifically on inertial navigation systems.[citation needed] She was Project Director of the Agni-V ICBM project.[citation needed]

Personal life

She is married to Saroj Kumar, a commander in the Indian Navy and they have a son,Tejas.[2]

Awards

Thomas received the Lal Bahadur Shastri National Award for her contribution for making India self-reliant in the field of missile technology.[3][4]

She was also the recipient of the Dr Thomas Cangan Leadership Award at the Faculty of Management Studies – Institute of Rural Management, Jaipur (FMS-IRM) in 2018.[5]

Thomas won 'Woman pioneer of the year' award at ETPrime Women Leadership Awards 2023 which was held at Mumbai.[6][7][8] The same year, she became a laureate of the Asian Scientist 100 by the Asian Scientist.[9]

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Publications

  • Thomas, Tessy (1 July 2005). "Guidance Scheme for Solid Propelled Vehicle during Atmospheric Phase". Defence Science Journal. 55 (3): 253–264. doi:10.14429/dsj.55.1987.
  • Sudhakar, R.; Venkanna, M.; Rao, B. V. Papa; Thomas, Tessy (2017). "Prediction of Real Gas and Non-Equilibrium Effects in the Gas Dynamics of Canister Launch Missile". 30th International Symposium on Ballistics. doi:10.12783/ballistics2017/16878. ISBN 978-1-60595-419-6.
  • Thomas, Tessy; Jahagirdar, D R; Krishna, I V Murali; Varaprasad, L. (May 2013). "Online Trajectory Reshaping for a Launch Vehicle to Minimize the Final Error Caused by Navigation and Guidance". Defence Science Journal. 63 (3). New Delhi: 254–261. doi:10.14429/dsj.63.2414. ProQuest 1413260295.
  • Ghogale, Shrikant; Venkanna, M.; Rao, B.V. Papa; Thomas, Tessy (2017). "Developmental Challenges during Realization of High Progressivity Rocket Motor". 30th International Symposium on Ballistics. doi:10.12783/ballistics2017/16860. ISBN 978-1-60595-419-6.
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See also

References

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