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151-0265-00L 4 Credits MSC D-MAVT
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Rocket Propulsion

VVZ CR n/a

Last Updated: 2026-02-05 15:13:53

Abstract

The objective of this new course is to introduce the students to the basic technology, performance, and design rationale of rocket propulsion. This subject is introduced through a discussion of the basic principles, a description of some of the physical mechanisms, and review of their principle applications.

Content

The course topics can be summarized as follows: Two-body orbital mechanics; Planetary orbits; Orbital elements, orbit determination and time of flight; Interplanetary transfers; Description and classifications of rocket engines; Rocket gas dynamic nozzle performance; Vehicle and booster performance with single and multi-staging; Liquid propellant rocket engine technology; Solid Propellant and hybrid rocket engines; Electric propulsion systems.

Resources

Lecture Notes

A script will be delivered before each session, in class, or be available for downloading from the course web page.

Literature

Francis J. Hale, Introduction to Space Flight, Prentice-Hall, 1994. Philip G. Hill and Carl R. Peterson, Mechanics and Thermodynamics of Propulsion, Addison-Wesley, 1992

General Information

Language
English
Levels
MSC
Frequency
Yearly recurring

Examination

Type
session examination
Mode
oral 30 minutes

Course Components

Type Title Time & Place Hours
lecture with exercise Rocket Propulsion
  • Tue 15:15-17:00 (CHN G 42)
  • Tue 17:15-18:00 (CHN G 42)
3 h weekly

Offered In