Dr Rajiv Kumar | Rocket Propulsion | Best Researcher Award

Dr Rajiv Kumar, Birla Institute of Technology, Mesra, Ranchi, India

Dr. Rajiv Kumar is a distinguished researcher and Assistant Professor in the Department of Space Engineering and Rocketry at Birla Institute of Technology, Mesra. He earned his Ph.D. in Hybrid Rocket Propulsion from IIT Madras, an M.E. in Rocket Propulsion from BIT Mesra, and a B.E. in Aeronautical Engineering from the Aeronautical Society of India. Specializing in propulsion technologies, his research addresses hybrid and solid rockets, combustion systems, and regression rate enhancement. With high-impact publications, multiple patents, and funded projects from DST-SERB and DRDO, Dr. Kumar’s innovative contributions significantly advance aerospace engineering and rocket propulsion. πŸš€βœ¨

Publication Profile

Scopus

Academic BackgroundπŸŽ“

Dr. Rajiv Kumar possesses an exceptional academic background in aerospace and propulsion engineering. πŸŽ“ He earned his Ph.D. in Hybrid Rocket Propulsion from the Indian Institute of Technology Madras, Chennai, in March 2014, with his defense held on February 12, 2014. πŸš€ Prior to this, he completed his M.E. in Rocket Propulsion from Birla Institute of Technology Mesra, Ranchi, in June 2007. πŸ”¬ Dr. Kumar began his journey with a B.E. in Aeronautical Engineering (Propulsion) from The Aeronautical Society of India, New Delhi, graduating in February 2005. ✈️ His expertise lies in advanced propulsion technologies for aerospace applications. 🌟

Professional Experience and Contributions πŸ’Ό

Dr. Rajiv Kumar has held key academic and research positions throughout his career. πŸŽ“ He worked as a Project Officer in the Department of Aerospace Engineering at the Indian Institute of Technology Madras from August 2011 to February 2014, contributing to advanced research in aerospace. πŸš€ Following this, he served as an Assistant Professor in the Department of Aeronautical Engineering at Vel Tech Dr. RR & Dr. SR Technical University, Avadi, from March 3, 2014, to March 26, 2015. 🏫 Since March 31, 2015, Dr. Kumar has been an Assistant Professor in the Department of Space Engineering and Rocketry at Birla Institute of Technology Mesra, Ranchi. 🌌

Research Focus Area 🌱🧬

Dr. Rajiv Kumar’s research primarily focuses on combustion and jet propulsion, with an emphasis on advanced propulsion technologies. πŸš€ His work covers propellant combustion, essential for optimizing the efficiency and performance of rocket systems. πŸ”₯ He also explores rocket and propellant technology, working on innovations to enhance aerospace propulsion systems. 🌠 Additionally, Dr. Kumar delves into heat transfer in aerospace propulsion systems, crucial for managing the thermal challenges in high-speed flight. 🌑️ His research extends to both air-breathing and non-air-breathing propulsion systems, advancing technologies for diverse aerospace applications. ✈️ His expertise plays a key role in improving propulsion efficiency and performance.

Award and Honours πŸ†

Dr. Rajiv Kumar has received numerous awards and honors throughout his career. πŸ† He serves as a reviewer for several prestigious journals, including Acta Astronautica, Combustion and Flame, and Journal of Aerospace Engineering. ✍️ Dr. Kumar has also been recognized for his contributions, receiving the Best Researchers Award in 2021 by Science Father and the Best Student Award in 1997. πŸŽ“ He has been invited to deliver lectures and motivational speeches at various international webinars and events, including the International Webinar on Rocket Propulsion and Aerospace Combustion workshop. 🌟 Additionally, he has contributed as a jury member for district and state-level competitions under the INSPIRE Award-MANAK Scheme. 🎀

Publication Top NotesπŸŒŸπŸ“ŠπŸ“š

Evaluation of combustion stability of single and multi-protrusion inserted hybrid rocket motor

Studies of Jet A1 Fuel Atomisation Through Non-Circular Orifices

Effect on the performance of a hybrid rocket using AP in the PVC and HTPB-based hybrid fuel

Development of hydrogen peroxide based micro thruster utilizing biomass-based catalyst bed

Performance estimation of hybrid rocket by varying the flow rate at multi-location swirl injector

Effect of Different Injectors on Performance of Hybrid Rocket Motor by Varying the L/D Ratio

Aging and Atomization Characteristics of Aluminum Loaded and Unloaded Ethanol Gel

Dr Rajiv Kumar | Rocket Propulsion | Best Researcher Award