ASE442 INTRODUCTION TO ROCKET TECHNOLOGY

Course Code:3840442
METU Credit (Theoretical-Laboratory hours/week):3 (3.00 - 0.00)
ECTS Credit:5.0
Department:Aerospace Engineering
Language of Instruction:English
Level of Study:Undergraduate
Course Coordinator:
Offered Semester:Fall Semesters.

Course Objectives

Apply the fundamentals to analyze the performance, motion, and the trajectories of rockets for various mission requirements and to design rockets for a specific mission. 


Course Content

This course provides introductory information for rocket/missile design, development, integration, operational characteristics and problems of full-scale missiles affected by the dynamics of environment. Determination, analysis and processing of missile trajectory including different flight conditions are discussed.


Course Learning Outcomes

Gain familiarity with rockets and propulsion system parts.

Apply the fundamentals of thermodynamics and compressible flow.

Become more aware of current topics in space propulsion. 

Learn nozzle types and nozzle flows, rocket vehicle types, engine cycles, types of propellants, combustion behavior of solid rocket propellants; and components of the liquid engine and solid motors, and their functions.

Be able to calculate rocket trajectories, rocket performance parameters, velocity increment requirements for basic missions (vertical launch, earth-to-orbit, and Hohmann transfer), the basic sizing, and staging of rockets.


Program Outcomes Matrix

Level of Contribution
#Program Outcomes0123
1ability to apply basic knowledge in mathematics, science, and engineering in solving aerospace engineering problems
2ability to analyze and design aerospace systems and subsystems
3ability to reach knowledge required to solve given problems and utilize that knowledge in solving them
4ability to follow advancements in their fields and improve themselves professionally
5ability to communicate and participate effectively in multi-disciplinary teams

0: No Contribution 1: Little Contribution 2: Partial Contribution 3: Full Contribution