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1) Course notes

2) Textbook: Hill, P., and Peterson, C., Mechanics and Thermodynamics of Propulsion, Addison-Wesley Publishing Co., 1992,

3) Any online material will be available at MyUni.

4) Digital recordings of lectures (e.g., taping lectures, wireless network, pod-casts) may not be made available to students who are absent.

1) Sutton, G. P., and Biblarz, O., Rocket Propulsion Elements, 8th Ed, Wiley-interscience, 2010

2) Bathie, W. W., Fundamentals of Gas Turbines, 2nd Ed, John Wiley & Sons, 1992.

3) Goebel, D. M, and Katz, I., Fundamentals of Electric Propulsion, John Wiley & Sons, 2008.

4) Turns, S. R., An Introduction to Combustion, 2nd Ed, McGraw-Hill, 2000.

Copies of assignments and any paper material distributed during class will also be posted on My-Uni.

Lectures supported by problem-solving tutorials, group seminars, and a practical laboratory developing material covered in lectures.

Formal Contact: Lectures and tutorials: 41 hours, Seminars: 4 hours, Practical: 5 hours, Exam: 3 hours.

Suggested personal workload (will vary between students): Reading and revising course material: 30-50 hours, Completion of assignments and practical report: 30-50 hours, Exam preparation: 30-50 hours.

The numbers quoted here are approximations and will vary if some activities take longer or less time than anticipated:

I. Review of thermodynamics and Introduction of Propulsion – 10 lectures

1. Review
2. Mixtures of gases
3. Thermodynamic cycles
4. Combustion thermodynamics

II. Chemical Propulsion – 24 lectures

1. Air-Breathing Propulsion Systems

1. turbojet systems
2. turbofan systems
3. turboprops/propfans systems
4. ramjet systems
5. scramjet systems
6. PDE’s and other advanced concepts

2. Air-Breathing Propulsion System Components

1. subsonic inlets and diffusers
2. supersonic inlets and diffusers
3. axial and radial (centrifugal) compressors
4. combustors
5. axial turbines
6. nozzles
7. propellors and fans

3. Air-Breathing Propulsion System Integration

4. Rocket Propulsion Systems

1. thrust analysis
2. vertical trajectory analyses
3. staging performance
4. basic orbital dynamics

5. Liquid propellant rocket systems

1. propellants
2. preburners
3. turbopumps
4. injectors
5. thrust chambers
6. nozzles

6. Solid propellant rocket systems

1. propellants
2. configurations
3. characteristics

III. Electric Propulsion – 5 lectures

1. Physics of electromagnetic fields
2. Plasmas and magnetohydrodynamics
3. One-dimensional steady flow of a plasma
4. Magnetic Reynolds number
5. Practical electric propulsion devices

IV. Alternative space propulsion systems (student Seminars) – 5 lectures

V. Review of course material – 2 lectures

Students will be required to adhere to laboratory conduct safety guidelines for the practical component of this course.

In order to pass this course, students must achieve a pass grade for the turbine engine performance laboratory.

• Final exam is a 3-hour long closed book exam, to be conducted during the formal university examination period.

• There will be 5 assignments in total. 4 of these are individual assignments (no collaboration) and the other is a group assignment/project. These will be distributed on MyUni. Due dates for these assignments may be subject to change; any changes will be announced via MyUni, written on the assignment, and posted on MyUni at the time the assignment is first distributed.

• The turbine engine performance laboratory is run as part of the formal Level IV laboratories.

Unless otherwise specified, submission of assignments and laboratory reports will be made through MyUni.

Extensions for assignments will only be given in exceptional circumstances and a case for this with supporting documentation must be made align with the MACA policy.

Assignments will be assessed and returned within 4 weeks from submission (usually significantly less) via MyUni. There will be no opportunities for re-submission of work of unacceptable standard. Due to the large class size, feedback on assignments will be limited to in-class discussion resulting from questions from students.