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Before choosing courseMJ2246 Rocket Propulsion 6.0 creditsAdministrate About course

Although rocket propulsion is a technology based on a physic law discovered on the XVI century, It experienced a strong development in the late century. Today, rocket propulsion is of paramount importance is space sciences, telecommunication and military applications.

In the Rocket Propulsion course the student will gain an insight into the physics behind rocket technology, propulsion systems, orbital mechanics, performance characteristics of propellants among others subjects.

Choose semester and course offering

Choose semester and course offering to see information from the correct course syllabus and course offering.

* Retrieved from Course syllabus MJ2246 (Autumn 2007–)

Content and learning outcomes

Course contents

Fundamentals of rocket vehicles: static performance, vehicle acceleration, orbital mechanics, types of rockets. Components of a rocket: performance characteristics, nozzle design. Chemical rocket propellants: performance with chemical equilibrium, non-equilibrium effects, combustion chamber design, hybrid rockets. Rocket engine subsystems: wall cooling, injectors, propellant feed systems, controls.

Projects: calculation of rocket nozzle flow field and calculation of liquid rocket performance with equilibrium chemistry

Intended learning outcomes

To provide an understanding of rocket propulsion systems for both launch and orbital control missions.

Course Disposition

50% selfstudy course with supportive lectures and seminar

Literature and preparations

Specific prerequisites

MJ1112 Thermodynamics, 9 hp or corresponding knowledge

SG1220 Fluid mechanics, 6 hp or corresponding knowledge

MJ2429 Turbomachinery, 6 hp or corresponding knowledge

Recommended prerequisites

Basic knowledge in thermodynamics and fluid mechanics is necessary

Equipment

No information inserted

Literature

Hill, P. and Peterson, R. 1992."Mechanics and Thermodynamics or Propulsion".

Addison-Wesley Publishing Company, Inc., USA. ISBN 0-201-14659-2. 

George P. Sutton, Oscar Biblarz, 2001“Rocket Propulsion Elements”, 7th Edition John-Wiley & Sons, Ltd., ISBN: 0-471-32642-9 Compedu (www.compedu.net)

Kungliga Tekniska Högskolan (KTH) - Sweden Department of Energy Technology

Division of Heat and Power Technology

Examination and completion

If the course is discontinued, students may request to be examined during the following two academic years.

Grading scale

A, B, C, D, E, FX, F

Examination

  • PRO1 - Project, 1,5 hp, betygsskala: P, F
  • TEN1 - Examination, 3,0 hp, betygsskala: A, B, C, D, E, FX, F
  • ÖVN1 - Home Assignments, 1,5 hp, betygsskala: P, F

Based on recommendation from KTH’s coordinator for disabilities, the examiner will decide how to adapt an examination for students with documented disability.

The examiner may apply another examination format when re-examining individual students.

Other requirements for final grade

PRO1 Project 1.5 hp         

TEN1 Examination 3.0 hp       

ÖVN1 Home Assignments 1.5
            

Opportunity to complete the requirements via supplementary examination

No information inserted

Opportunity to raise an approved grade via renewed examination

No information inserted

Examiner

Profile picture Björn Laumert

Ethical approach

  • All members of a group are responsible for the group's work.
  • In any assessment, every student shall honestly disclose any help received and sources used.
  • In an oral assessment, every student shall be able to present and answer questions about the entire assignment and solution.

Further information

Course web

Further information about the course can be found on the Course web at the link below. Information on the Course web will later be moved to this site.

Course web MJ2246

Offered by

ITM/Energy Technology

Main field of study

Mechanical Engineering

Education cycle

Second cycle

Add-on studies

No information inserted

Contact

Björn Laumert, bjorn.laumert@energy.kth.se