{"id":58846,"date":"2023-09-05T13:15:35","date_gmt":"2023-09-05T13:15:35","guid":{"rendered":"https:\/\/www.inspirenignite.com\/anna-university\/as3015-spacecraft-structures-syllabus-for-aerospace-engg-2021-regulation-professional-elective-vi\/"},"modified":"2023-09-05T13:15:35","modified_gmt":"2023-09-05T13:15:35","slug":"as3015-spacecraft-structures-syllabus-for-aerospace-engg-2021-regulation-professional-elective-vi","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/as3015-spacecraft-structures-syllabus-for-aerospace-engg-2021-regulation-professional-elective-vi\/","title":{"rendered":"AS3015: Spacecraft Structures syllabus for Aerospace Engg 2021 regulation (Professional Elective-VI)"},"content":{"rendered":"

Spacecraft Structures 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-VI scheme and its subjects refer to Aerospace Engg Professional Elective-VI syllabus scheme<\/a>. The detailed syllabus of spacecraft structures is as follows. <\/p>\n

Course Objectives:<\/h4>\n

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Unit I<\/h4>\n

SPACECRAFT DESIGN LOADS
\nTransportation load factors – Steady-State Loads – Mechanical Dynamic loads – Acoustic loads -Shock loads – Static pressure variations – Micro-meteorites \/ Orbital Debris.\n<\/p>\n

Unit II<\/h4>\n

DESIGN OF SPACECRAFT STRUCTURE
\nIntroduction – Determination of Spacecraft Configuration – First Design Spacecraft Structure -Basic Design Supporting Structure – Detailed Analyses – Manufacturing of the spacecraft structure.\n<\/p>\n

Unit III<\/h4>\n

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Unit IV<\/h4>\n

FATIGUE LIFE PREDICTION
\nIntroduction – Palmgren-Miner Linear Cumulative Damage Rule – Analysis of Load-time Histories – Failure due to Sinusoidal Vibrations – Failure due to Narrow-banded Random Vibrations.\n<\/p>\n

Unit V<\/h4>\n

DAMAGE TO SPACECRAFT BY METEOROIDS AND ORBITAL DEBRIS9
\nIntroduction – Micro-Meteoroids and Space Debris Environment – Micro-Meteoroids Environment – Orbital debris Environment – Hyper Velocity Impact Damage Models – Single Plate Penetration Equations – Multi-shock shield – Probability of Impacts.\n<\/p>\n

Course Outcomes:<\/h4>\n

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