Description of Individual Course Units
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Offered By |
Faculty of Engineering |
Level of Course Unit |
First Cycle Programmes (Bachelor's Degree) |
Course Coordinator |
PROFESSOR DOCTOR ŞAHIN YAVUZ |
Offered to |
Mechanical Engineering (Evening) |
Course Objective |
This course aims to teach the fundamental principles and engineering approaches used in the thermal design and analysis of satellite launch vehicles. Students will learn to understand the thermal challenges of the space environment, design thermal control systems, and analyze these systems using modern software. The course aims to develop students' competence in aerospace engineering by supporting theoretical knowledge with practical applications and industrial examples. |
Learning Outcomes of the Course Unit |
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Mode of Delivery |
Face -to- Face |
Prerequisites and Co-requisites |
None |
Recomended Optional Programme Components |
None |
Course Contents |
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Recomended or Required Reading |
- Gilmore, D. G. (2002). Spacecraft Thermal Control Handbook: Fundamental Technologies, AIAA |
Planned Learning Activities and Teaching Methods |
Upon successful completion of this course, students will be able to: |
Assessment Methods |
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Further Notes About Assessment Methods |
None |
Assessment Criteria |
Midterm %25 + Homework %25 + Final %50 |
Language of Instruction |
Turkish |
Course Policies and Rules |
To be announced. |
Contact Details for the Lecturer(s) |
sahin.yavuz@deu.edu.tr |
Office Hours |
will be announced. |
Work Placement(s) |
None |
Workload Calculation |
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Contribution of Learning Outcomes to Programme Outcomes |
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