The main objective of this course is to
- teach students fundamental knowledge about rocket systems and spacecraft propulsion systems,
- educate them how to apply this knowledge for space vehicle propulsion,
- encourage them to do research in space propulsion.
Course content:
Aerothermodynamic performance evaluation of air and spacecraft propulsive systems. Rocket propulsion with solid, liquid and hybrid propellant systems. Chemistry of combustion. Burning rates for solid and liquid propellants, components of solid and liquid rocket engines. Flight performance, maneuver and attitude control for spacecraft. Rocket propulsion system design and selection. Rocket exhaust plumes and its effects. Rocket testing.