AE3852 Propulsion for Launch Vehicles

Introduction to propulsion for launch vehicles, beginning with mission energy requirements and an overview of current and proposed launch propulsion devices. Performance analysis, operating characteristics and propellant selection criteria are considered for air breathing and solid, liquid and nuclear rocket motor propulsion systems. Advanced cycles and concepts are presented. Design of components and subsystems.

Prerequisite

ME3201

Lecture Hours

4

Lab Hours

0

Course Learning Outcomes

Understanding of Propulsion Principles: Gain a comprehensive understanding of the fundamental principles of propulsion, including thermodynamics, combustion processes, and propulsion systems specific to launch vehicles.

Analysis of Engine Performance: Analyze the performance characteristics of different types of rocket engines, including liquid propulsion systems (such as RP-1/LOX and LH2/LOX) and solid rocket motors, considering factors such as specific impulse, thrust-to-weight ratio, and efficiency.

Design and Optimization: Develop skills in the design and optimization of propulsion systems for launch vehicles, considering factors such as engine cycle selection, nozzle design, and propellant choices to meet specific mission requirements.

Integration with Launch Vehicles: Understand the integration of propulsion systems with overall launch vehicle design, including considerations for structural dynamics, aerodynamics, and vehicle stability.

Safety and Reliability: Evaluate safety and reliability aspects of propulsion systems, including failure modes analysis, risk assessment, and mitigation strategies to ensure mission success and crew safety.

Advanced Propulsion Concepts: Explore advanced propulsion concepts such as electric propulsion, nuclear thermal propulsion, or alternative propulsion technologies, and assess their potential applications and challenges for launch vehicles.