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At the end of the course the learners can estimate the energy required for a rocket launch vehicle to meet the given mission specifications, fix the number of stages with(out) boosters, select liquid engine or solid motor configurations and calculate various design parameters and estimate performance of engine or launch vehicle.
Goteti hold a doctorate degree in Mechanical Engineering. He has worked as Propulsion Engineer and involved in the design of liquid rocket engines (LRE) at Indian Space Research Organization (ISRO), India. Goteti have worked with multinational companies in design and manufacturing of pressure vessels and thermal equipments like heat exchangers and solar thermal energy equipment. As a professor of Mechanical Engineering in an Indian University, where he taught Aerospace and Thermal Engineering subjects to graduate students. Goteti is always available and happy to share my knowledge and experience with inquisitive learners.
Dr. Goteti Satyanarayana - Consultant Engineer