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Dr. Syed Alay Hashim

Associate Professor

Alliance College of Engineering and Design

Dr. S. A. Hashim earned his Ph.D. from the Department of Aerospace Engineering, IIT Kharagpur. His expertise lies in the area of Aerospace with specialization in aircraft and rocket propulsion. During his Ph.D. at IIT Kharagpur, he established systems for processing and testing of hybrid fuel and propellants. He has about over a decade of experience in both teaching and research. His research includes ducted rocket propulsion, micro gas turbine, ramjet, pulsejet engine etc.

Dr. Hashim has published research articles in combustion and propulsion journals such as Combustion and Flame, Propellants, Explosives, Pyrotechnics, Acta Astronautica, Combustion Science and Technology, Journal of Spacecraft and Rockets/AIAA, and so on. His research has direct relevance in development of boron-based high-energy and high-density hybrid fuels and propellants for air-breathing propulsion systems in missile applications.

Journal Papers

  • Hashim, S.A., Islam, M., Kangle, S., Karmakar, S., and Roy, A. (2020). Performance evaluation of boron/hydroxyl-terminated polybutadiene-based solid fuels containing activated charcoal. Journal of Spacecraft and Rockets/AIAA Journal, 58(2) 363-374.
  • Hashim, S.A., Karmakar, S., and Roy, A. (2019). Experimental observation and characterization of B–HTPB-based solid fuel with addition of iron particles for hybrid gas generator in ducted rocket applications. Propellants, Explosives, Pyrotechnics, 44(7), 896-907.
  • Hashim, S.A., Karmakar, S., and Roy, A. (2019). Effects of Ti and Mg particles on combustion characteristics of boron–HTPB-based solid fuels for hybrid gas generator in ducted rocket applications. Acta Astronautica, 160, 125–137. (Top 10/IIT KGP)
  • Hashim, S.A., Karmakar, S., and Roy, A. (2018). Combustion characteristics of boron-HTPB-based solid fuels for hybrid gas generator in ducted rocket applications. Combustion Science and Technology, 191(11), 2082–2100.
  • Hashim, S.A., Karmakar, S., Roy, A., and Srivastava, S.K. (2018). Regression rates and burning characteristics of boron-loaded paraffin-wax solid fuels in ducted rocket applications. Combustion and Flame, 191, 287-297. (Top 10/IIT KGP)
  • Hashim, S.A. (2013). Design and fabrication of an annular combustion chamber for the micro gas turbine engine applications. International Journal of Engineering Research & Technology, 2(8), 1307-1314.
  • Hashim, S.A., Manish, P.N., and Naresh, K. (2013). Low NOx emission with improved performance of the gas turbine engine. International Journal of Engineering Research & Technology, 2(11), 758-762.
  • Hashim, S.A., Grover, U., Dixit, P., and Davis, S. (2013). Characterization of Hokuyo Laser rangefinders in terms of material recognition. International Journal of Engineering Research & Technology, 2(10), 1003-1009.

Book Chapters

  • Hashim, S.A., Karmakar, S., Roy, A., and Sheikh, S. (2020). Performance evaluation of boron particles with wax–HTPB-based solid fuel for the primary combustor in ducted rocket applications. Increasing Role of Indian Aerospace Industries for Aeronautics, Space Projects and Systems. Annual Technical Volume of Aerospace Engineering Division Board, Increasing Role of Indian Aerospace Industries for Aeronautics, Space Projects and Systems. The Institution of Engineers India, 4, 91-98. (ISBN 978-81-950662-4-7)
  • Hashim, S.A., Karmakar, S., Roy, A., and Sheikh, S. (2020). Performance evaluation of boron particles with wax–HTPB-based solid fuel for the primary combustor in ducted rocket applications. National Conference on Emerging Technologies in Aerospace Structures, Materials and Propulsion Systems. The Institution of Engineers Pune, India, 7-13. (ISBN 978-81-942561-9-9)
  • Hashim, S.A., Kangle, S., Karmakar, S., and Roy, A. (2018). Performance augmentation of boron-HTPB based solid fuels by energetic additives for hybrid gas generator in ducted rocket applications. Innovative Design and Development Practices in Aerospace and Automotive Engineering. Springer Singapore, 143-157. (ISBN 978-981-13-2697-4)
  • Hashim, S.A., Lahariya M., Karmakar, S., and Roy, A. (2016). Calculation of theoretical performance of boron-based composite solid propellant for the future applications. Innovative Design and Development Practices in Aerospace and Automotive Engineering. Springer Singapore, 327–335. (ISBN 978-981-10-1771-1)
  • Hashim, S.A., Manish, N., Mishra, D., and Ahuja, K. (2014). Reduction of the passage between the flame tubes of the combustor for a millimeter size gas turbine engine in the art of micromachine technology. Innovative Design and Development Practices in Aerospace and Automotive Engineering. Springer Singapore, 197–205. (ISBN 978-81-322-1871-5)

Awards
  • Best Researcher Award 2021 in the 26th International Scientist Awards on Engineering, Science, and Medicine by VDGOOD Professional Association, India.
  • MHRD, Govt. of India fellowship.
  • Best publication award by Aerospace department/IIT Kharagpur for the papers in Top10 journals.
  • Best faculty Award by Sandip University Nashik, Maharastra, India.
  • Krishnan Award for securing highest marks in India (2004) in Propulsion-II paper (Aircraft Propulsion).
Member of Professional Bodies
  • Life member of The Aeronautical Society of India
  • Associate member of The Institution of Engineers India

Conference Proceedings
  • Sheikh, S., Shubham, P., Hashim, S.A., Karmakar, S., and Roy, A. (2020). Design and testing of missile launcher-based drone for defense applications. International Conference, AeSI-2020 on Aviation Technology- Current Scenario, The Aeronautical Society of India, Kolkata branch.
  • Hashim, S.A., Karmakar, S., Roy, A., and Sheikh, S. (2019). Performance evaluation of boron particles with wax–HTPB-based solid fuel for the primary combustor in ducted rocket applications. National Conference on Emerging Technologies in Aerospace Structures, Materials and Propulsion Systems, The Institution of Engineers Pune branch, India.
  • Hashim, S.A., Islam, M., Karmakar S., and Roy A. (2018). Effects of iron particles on boron–HTPB-based solid fuel for SFDR applications using rapid screening instrument, National Aerospace Propulsion Conference, NAPC, IIT Kharagpur, India.
  • Hashim, S.A., Kangle, S., Karmakar, S., and Roy, A. (2018). Screening of nano-aluminum based solid fuels for the hybrid rocket applications,” The American Institute of Aeronautics and Astronautics, AIAA Aerospace Sciences Meeting, Florida, USA.
  • Hashim, S.A., Kangle, S., Karmakar, S., and Roy, A. (2018). Performance augmentation of boron-HTPB based solid fuels by energetic additives for hybrid gas generator in ducted rocket applications. Innovative Design and Development Practices in Aerospace and Automotive Engineering, I-DAD, VTU, Chennai, India.
  • Hashim, S.A., Kangle, S., Karmakar, S., and Roy A. (2017). Screening of boron-based solid fuels for hybrid rocket applications, High Energy Material Conference and Exhibits (HEMCE), DRDO Pune, India.
  • Hashim, S.A., Kangle, S., Karmakar, S., and Roy A. (2017). Combustion characteristics of boron-HTPB based solid fuels for hybrid rocket applications, International Conference on Theoretical, Applied, Computational and Experimental Mechanics, ICTACEM, IIT Kharagpur, India.
  • Hashim, S.A., Lahariya, M., Karmakar, S., and Roy, A. (2016). Calculation of theoretical performance of boron-based composite solid propellant for the future applications, Innovative Design, Analysis and Development Practices in Aerospace and Automotive Engineering, I-DAD, VTU, Chennai, India.
  • Hashim, S.A., Manish, N., Mishra, D., and Ahuja, K. (2014). Reduction of the passage between the flame tubes of the combustor for a millimeter size gas turbine engine in the art of micromachine technology, Innovative Design, Analysis and Development Practices in Aerospace and Automotive Engineering, I-DAD, VTU, Chennai, India.
  • Hashim, S.A., Manish, N., Peter, P., Ahuja, K., and Grover, U. (2013). Low NOx emission at maximum efficiency of the gas turbine engine, Recent trends in applied chemistry (RTAC), VTU Chennai, India.
  • Hashim, S.A. (2009). Setting up of rocket propellant processing facility, Fligen Aero Fest, PCET Coimbatore, India.