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Addresses: School of Mechanical Engineering, Iran University of Science & Technology, Narmak, Tehran, Iran

Zip Code: 16846-13114

Mail Box: 16765-163

Tel : +98(21) 77491228-29

Fax : +98(21) 77240488

Email: meresearch@iust.ac.ir

:: Course Modules- M.Sc-Aerospace ::

  Department of aerospace engineering

  Objective of this department is to create ability in research, design, manufacturing and test of aerospace systems in divisions of propulsion, aerodynamics, structure, dynamics and control of space systems.

  Aero systems such as airplane, helicopter and rockets as well as space systems such as satellites are based on advanced and modern technologies. Ability in design and manufacturing of these systems is tantamount to advancements in national technological, economical and defense achievements.

  In addition, science and technology in aerospace as a progressive industry can assist other areas such as turbo-compressors used in gas pumping stations, automotive technologies, underground tunnels, industrial motors as well as construction.

  In graduate programs, advanced methods in mathematical modeling, analysis, control, design, manufacturing and testing of different elements of aerospace systems are taught in approved formats by the department. Moreover, by completing seminars and thesis in the planned curriculum of different majors within the department, students will be prepared to face the real applications of their learning within the industry.


  Aerospace field courses


  Mandatory courses: 18 Units

  Advanced mathematics: 3 Units

  Advanced numerical calculation: 3 Units

  Mandatory-optional courses: 4 Courses from following: 12 Units


  Aerospace structure field:


  Supersonic Aerodynamics:

  3 Units

  Structure Dynamics: 3 Units

  Advanced Propulsion Fundamental: 3 Units

  Subsonic Aerodynamics:

  3 Units

  Analysis of Advanced Aerospace Structure: 3 Units

  Design of Turbo Machine Aerodynamic: 3 Units

  Advanced Aerodynamics:

  3 Units

  Finite Elements Method:

  3 Unit

  Advanced Combustion:

  3 Units

  Calculating fluid dynamics:

  3 Units

  Advanced Design of Space Vehicle: 3 Units

  Entrance Aerodynamics:

  3 Units

  Boundary layer theory:

  3 Units

  Advanced Space Structure Design: 3 Units

  Missile engines Aerothermodynamics:

  3 Units

  Elective courses: 6 Units from other courses of various fields Aerospace

  Seminar: 2 Units

  Project: 6 Units

  Total: 32 Units

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