Spacecraft Power Technologies detail syllabus for Electrical Engineering (EEE), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17EE753), and for exam duration, Teaching Hr/week, Practical Hr/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below.
For all other eee 7th sem syllabus for be 2017 scheme vtu you can visit EEE 7th Sem syllabus for BE 2017 Scheme VTU Subjects. For all other Professional Elective-4 subjects do refer to Professional Elective-4. The detail syllabus for spacecraft power technologies is as follows.
Course Objectives:
- To discuss the increasing demand for space craft power systems and to give an overview of electrical power system and its technology.
- To discuss near – earth environmental factors that will affect the design of space craft power systems.
- To describe the elements of a space photovoltaic power system, the status of solar cell technologies presently in use.
- To discuss advances in both cell and array technology, and solar thermo photovoltaic energyconversion.
- To discusses, space-qualified components, the array of chemical storage technologies including both batteries and fuel cells.
- To describe components and techniques for achieving the various Power Management and Distribution functions and examples of several PMAD configurations.
Module 1
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Module 2
Solar Energy Conversion: Introduction, Solar Cell Fundamentals, Space Solar Cell Calibration and Performance Measurements, Silicon Space Solar Cells, III-V Compound Semiconductor Solar Cells, Thin Film Solar Cells.
Module 3
Solar Energy Conversion (continued):Space Solar Cell Arrays, Space Thermo photovoltaic Power Systems. Chemical Storage and Generation Systems: Introduction, Inventions, Evolution of Batteries in Space, Fundamentals of Electrochemistry, Cell and Battery Mechanical Design, Performance Metrics.
Module 4
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Module 5
Power Management and Distribution (PMAD): Introduction, Functions of PMAD, Components and Packaging, System Examples.
Course Outcomes:
At the end of the course the student will be able to:
- Discuss the increasing demand for space craft power systems and to give an overview of electrical power system and its technology.
- Discuss near – earth environmental factors that will affect the design of space craft power systems
- Describe the elements of a space photovoltaic power system, the status of solar cell technologies presently in use.
- Discuss advances in both cell and array technology, and solar thermo photovoltaic energy conversion.
- Discusses, space-qualified components, the array of chemical storage technologies including both batteries and fuel cells.
- Describe components and techniques for achieving the various Power Management and Distribution functions and examples of several PMAD configurations.
Graduate Attributes (as per NBA):
- Engineering Knowledge,
- Problem Analysis,
- Design/ Development of Solutions,
- Conduct investigations of complex problems,
- Modern Tool Usage,
- Ethics,
- Individual and Team Work,
- Communication,
- Life-long Learning
Question paper pattern:
- The question paper will have ten questions.
- Each full question is for 16 marks.
- There will be 2full questions (with a maximum of four sub questions in one full question) from each module.
- Each full question with sub questions will cover the contents under a module.
- Students will have to answer 5 full questions, selecting one full question from eachmodule.
Text Books:
- Spacecraft Power Technologies A.K. Hyder et al Imperial College Press 1st Edition, 2000
Reference Books:
- Spacecraft Power Systems Mukund R. Patel CRC Press 1st Edition, 2004
For detail syllabus of all other subjects of BE Eee, 2017 regulation do visit Eee 7th Sem syllabus for 2017 Regulation.
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