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COURSE PRO FORMA




             IMPORTANT:

             Contents of this Pro Forma shall not be changed without the Senate’s approval for items indicated with *. Changes
             to the other items can be approved at the Academy/Faculty/Institution/Centre level.


             Academy/Faculty/Centre                Faculty of Engineering

             Department                            Department of Mechanical Engineering

             Programme                             Bachelor of Engineering (Mechanical)



             Course Code*                          KMEM4368

             Course Title*                         Aerospace Propulsion Systems

             Course Pre-requisite(s)/ Minimum Require-  KMEM1108  Fundamentals of Fluid Mechanics
             ment(s)                               KMEM1109  Thermodynamics


             Student Learning Time (SLT)*          120

             Credit*                               3

             Learning Outcomes*                    At the end of this course students will be able to:
                                                   1.  Confidently explain, discuss, and assess propulsion systems and test
                                                      data with professional engineers.
                                                   2.  Analyze the component and system performance of rockets, aero pis-
                                                      ton engines, gas turbine engines, and ramjets.
                                                   3.  Produce a conceptual design or make improvement modifications to an
                                                      existing propulsion system.
             Transferable Skills                   Critical  thinking,  problem  solving,  design,  communication,  and  cohesive
                                                   team work


             Synopsis of Course Contents           This course introduces the propulsion systems used in modern aerospace
                                                   systems  (e.g.  aircraft,  missiles,  space  launchers,  etc.).  Systems  include:
                                                   rockets,  piston  aero-engines,  gas  turbine  engines  (e.g.  turbofans,  turbo-
                                                   props,  turboshafts,  etc.),  ramjets  and  scramjets.  Students  will  study  and
                                                   analyze the specific components of these systems. They will perform math-
                                                   ematical engineering analysis on different types of propulsion elements and
                                                   calculate their effect on the overall system performance using industry de-
                                                   rived figures of merit. Students will be required to work in teams to produce
                                                   an integrated conceptual design of a propulsion system optimized to meet
                                                   specified mission requirements.
             Method of Delivery (lecture, tutorial, work-  Lecture, Active Learning (AL), Cooperative Learning (CL), Group Project
             shop, etc)

             Assessment Methods*                   Continuous assessment: 100%, Final exam: None (0%)
                                                   (Tests, 50%, Assignments, 10%, Group Project, 40%)
             Methodologies for Feedback on Perfor-
             mance                                 During lectures, individual assignments, announcements

             Criteria in Summative Assessment      Refer  to  Kaedah-Kaedah  Universiti  Malaya  (Pengajian  Ijazah  Pertama)
                                                   2013  Peraturan-Peraturan  Universiti  Malaya  (Pengajian  Ijazah  Pertama)
                                                   2013

               UM-PT01-PK03-BR003(BI)-S04
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