The Department has state of the art experimental facilities in Aerodynamics and Rocket propulsion. Laboratories include low speed and supersonic wind tunnels, static rocket test facility for solid, liquid and hybrid rockets. Apart from these, rocket propulsion lab has facilities such as low and high pressure burning rate facilities for solid propellant, ignition and combustion facility for liquid and hybrid propellants, propellant processing lab., combustion and thermal analysis lab. etc.
Detailed information can be found in the section of this site devoted to Research, Facilities, and Laboratory Facilities.