Anna University Syllabus - Anna University ME Syllabus
AS7203 SPACECRAFT POWER SYSTEMS Syllabus | Anna University ME Aerospace Technology Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Aerospace Technology(Launch Vehicle Technology), Textbooks, Reference books, Exam portions, Question Bank, Previous year question papers, Model question papers, Class notes, Important 2 marks, 8 marks, 16 marks topics.
It is applicable for all students admitted in the Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.
Anna University Chennai Syllabus
AS7203 SPACECRAFT POWER SYSTEMS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, students will understand the advanced concepts of Spacecraft power
systems and to provide the necessary mathematical knowledge that are needed in modeling the
navigation process and methods. The students will have an exposure on various Power system
elements,energy storage technology and power converters and will be able to deploy these skills
effectively in the analysis and understanding of power systems in an spacecraft.
UNIT I SPACECRAFT ENVIRONMENT & DESIGN CONSIDERATION 9
Orbit definition /Mission Requirements of LEO, GEO, GTO & HEO, Lunar orbits, IPO with respect to
Power Generation – Power System Elements - Solar aspect angle Variations
UNIT II POWER GENERATION 9
Study of Solar spectrum - Solar cells - Solar Panel design - Solar Panel Realization – Solar Panel
testing - Effects of Solar cells and panels (IR, UV, Particles)
UNIT III ENERGY STORAGE TECHNOLOGY 9
Types of batteries – Primary & Secondary batteries - Nickel Cadmium - Nickel-Hydrogen – Nickel
metal hydride - Lithium-ion –Lithium Polymer - Silver Zinc– Electrical circuit model – Performance
characteristics of batteries - Application of batteries in launch vehicles and satellites – Fuel Cell –
Polymer Electrolyte membrane Fuel Cell – Regenerative Fuel Cell
UNIT IV POWER CONVERTERS 9
DC – DC converters – Basic Convertors - Buck, Boost, Buck- boost converter –Derived converters:
Fly back converter – Transformer coupled forward converter – Push-Pull converter - CUKs convertor–
Resonant converter – Voltage and current regulators
UNIT V POWER CONTROL, CONDITIONING AND DISTRIBUTION 9
Solar Array Regulators – Battery changing schemes – Protection Schemes - Distribution – Harness -
Thermal Design - EMI/EMC/ESD/Grounding schemes for various types of circuits and systems
L : 45, TOTAL: 45 PERIODS
REFERENCES
1. P R K Chetty, ‘Spacecraft Power Systems’, 1978.
2. Patel, Mukund R, ‘Spacecraft Power Systems’ CRC Press Boca Raton, 2005
3. Hyder, A k et.al, ‘ Space Power Technologies’ Imperial College Press London,2000
4. Fortescue, Peter et.al, ‘ Spacecraft Systems Engineering’ John Wiley England,2003.
5. Ned Mohan, et al,” Power Electronics, convertors Applications and Design”
AS7203 SPACECRAFT POWER SYSTEMS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, students will understand the advanced concepts of Spacecraft power
systems and to provide the necessary mathematical knowledge that are needed in modeling the
navigation process and methods. The students will have an exposure on various Power system
elements,energy storage technology and power converters and will be able to deploy these skills
effectively in the analysis and understanding of power systems in an spacecraft.
UNIT I SPACECRAFT ENVIRONMENT & DESIGN CONSIDERATION 9
Orbit definition /Mission Requirements of LEO, GEO, GTO & HEO, Lunar orbits, IPO with respect to
Power Generation – Power System Elements - Solar aspect angle Variations
UNIT II POWER GENERATION 9
Study of Solar spectrum - Solar cells - Solar Panel design - Solar Panel Realization – Solar Panel
testing - Effects of Solar cells and panels (IR, UV, Particles)
UNIT III ENERGY STORAGE TECHNOLOGY 9
Types of batteries – Primary & Secondary batteries - Nickel Cadmium - Nickel-Hydrogen – Nickel
metal hydride - Lithium-ion –Lithium Polymer - Silver Zinc– Electrical circuit model – Performance
characteristics of batteries - Application of batteries in launch vehicles and satellites – Fuel Cell –
Polymer Electrolyte membrane Fuel Cell – Regenerative Fuel Cell
UNIT IV POWER CONVERTERS 9
DC – DC converters – Basic Convertors - Buck, Boost, Buck- boost converter –Derived converters:
Fly back converter – Transformer coupled forward converter – Push-Pull converter - CUKs convertor–
Resonant converter – Voltage and current regulators
UNIT V POWER CONTROL, CONDITIONING AND DISTRIBUTION 9
Solar Array Regulators – Battery changing schemes – Protection Schemes - Distribution – Harness -
Thermal Design - EMI/EMC/ESD/Grounding schemes for various types of circuits and systems
L : 45, TOTAL: 45 PERIODS
REFERENCES
1. P R K Chetty, ‘Spacecraft Power Systems’, 1978.
2. Patel, Mukund R, ‘Spacecraft Power Systems’ CRC Press Boca Raton, 2005
3. Hyder, A k et.al, ‘ Space Power Technologies’ Imperial College Press London,2000
4. Fortescue, Peter et.al, ‘ Spacecraft Systems Engineering’ John Wiley England,2003.
5. Ned Mohan, et al,” Power Electronics, convertors Applications and Design”
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