Course Description
M. E. in Space Engineering and Rocketry with top to bottom specialization in two explicit territories to be specific Aerodynamics and Rocket Propulsion. The Department expects to give a condition of craftsmanship instruction and preparing to its students to empower them to contribute proficiently in the National endeavours being made in the fields of Space and Defence-related advancements and testing future missions. The Department likewise gives inquire about offices at doctoral and postdoctoral levels in the fields of Aerodynamics and Flow Studies, Propellant Technology, Rocket Propulsion and Combustion. The Rocket Propulsion Laboratory has static test set-ups outfitted with a PC controlled terminating office and PC based information procurement and examination framework for strong, fluid and half and half rocket engines. The fundamental framework for plan and creation of rocket engines is likewise accessible in the Department. In the territory of Propellant Technology, complete handling and portrayal offices are accessible for rocket charges and igniters. Propelled systems and types of gear for doing research in the zones of high-vitality materials, igniters, inhibitors and separators, and elite metalized gelled charges are likewise accessible in the Department. Present-day types of gear like STA, TGA, DSC, Viscometers, Rheometers, Calorimeters Spectrophotometers Flame Propagation and Stability Unit and so on are accessible for preparing and research.