{"id":58838,"date":"2023-09-05T13:15:15","date_gmt":"2023-09-05T13:15:15","guid":{"rendered":"https:\/\/www.inspirenignite.com\/anna-university\/as3010-spacecraft-systems-engineering-syllabus-for-aerospace-engg-2021-regulation-professional-elective-v\/"},"modified":"2023-09-05T13:15:15","modified_gmt":"2023-09-05T13:15:15","slug":"as3010-spacecraft-systems-engineering-syllabus-for-aerospace-engg-2021-regulation-professional-elective-v","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/as3010-spacecraft-systems-engineering-syllabus-for-aerospace-engg-2021-regulation-professional-elective-v\/","title":{"rendered":"AS3010: Spacecraft Systems Engineering syllabus for Aerospace Engg 2021 regulation (Professional Elective-V)"},"content":{"rendered":"

Spacecraft Systems Engineering detailed syllabus for Aerospace Engineering (Aerospace Engg) for 2021 regulation curriculum has been taken from the Anna Universities<\/a> official website and presented for the Aerospace Engg students. For course code, course name, number of credits for a course and other scheme related information, do visit full semester subjects post given below. <\/p>\n

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme<\/a>. For Professional Elective-V scheme and its subjects refer to Aerospace Engg Professional Elective-V syllabus scheme<\/a>. The detailed syllabus of spacecraft systems engineering is as follows. <\/p>\n

Course Objectives:<\/h4>\n

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Unit I<\/h4>\n

SPACECRAFT STRUCTURES
\nDeployment and Geometry Maintenance – Deployment for Aperture Maintenance – Origins Telescope Dynamics and Controls – SIM Dynamics and Control Block Diagram – Dynamic Disturbance Sources – Disturbance Analysis – Modal Sensitivity Analysis – Thermal Issues with Structures – Impedance Matched Tether Termination – Control-Structure Interaction – SPECS Geometry – Tether Vibration Control.\n<\/p>\n

Unit II<\/h4>\n

SPACECRAFT POWER SYSTEMS
\nElectrical Power System – Power Sources – Power Source Applicability – Design Space for RTGs -Primary Battery Types – Secondary Battery Types – Depth of Discharge – Fuel Cells and Characteristics – Radioisotope Thermoelectric Generators – Thermoelectric Generator – Solar Cell -Solar Cell Physics – Solar Cell Operating Characteristics – Temperature Effects – Radiation Effects – Solar Array Construction – Cell Shadowing – Power Distribution Systems – DET Power Regulation Systems – PPT Power Distribution Systems.\n<\/p>\n

Unit III<\/h4>\n

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Unit IV<\/h4>\n

SATELLITE COMMUNICATION SYSTEM
\nSatellite Communications Architecture – Advantages of Digital Communication – Data Collection Mission – Link Design Process – Power Flux Density – Received Power – System Noise Temperature – Modulation Techniques – Bit Error Rate – Convolutional Coding with Viterbi Decoding – Attenuation – Frequency Selection Drivers – Multiple Access Strategies – Antijam Techniques – Differential Pulse Code Modulation (DPCM).\n<\/p>\n

Unit V<\/h4>\n

LAUNCH SYSTEMS
\nLaunch System Selection Process – Launch Sites Criteria – Payload Integration – Fairings -Structural & Electrical Interface – Payload Environments – Acceleration Load Factors – Vibration Environments – Shock Loads – Acoustic Environments – Injection Accuracy – Payload Integration Procedures – Payload Processing – Launch System Cost Estimate.\n<\/p>\n

Course Outcomes:<\/h4>\n

On successful completion of this course, the student will be able to<\/p>\n