{"id":58811,"date":"2023-09-05T13:14:09","date_gmt":"2023-09-05T13:14:09","guid":{"rendered":"https:\/\/www.inspirenignite.com\/anna-university\/as3005-launch-vehicle-configuration-design-syllabus-for-aerospace-engg-2021-regulation-professional-elective-i\/"},"modified":"2023-09-05T13:14:09","modified_gmt":"2023-09-05T13:14:09","slug":"as3005-launch-vehicle-configuration-design-syllabus-for-aerospace-engg-2021-regulation-professional-elective-i","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/as3005-launch-vehicle-configuration-design-syllabus-for-aerospace-engg-2021-regulation-professional-elective-i\/","title":{"rendered":"AS3005: Launch Vehicle Configuration Design syllabus for Aerospace Engg 2021 regulation (Professional Elective-I)"},"content":{"rendered":"

Launch Vehicle Configuration Design 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 5th Sem scheme and its subjects, do visit Aerospace Engg 5th Sem 2021 regulation scheme<\/a>. For Professional Elective-I scheme and its subjects refer to Aerospace Engg Professional Elective-I syllabus scheme<\/a>. The detailed syllabus of launch vehicle configuration design is as follows. <\/p>\n

Course Objectives:<\/h4>\n

Download the iStudy App for all syllabus and other updates.<\/a>
\"Get<\/a><\/h4>\n

Unit I<\/h4>\n

FUNDAMENTAL ASPECTS
\nEnergy and Efficiencies of power plants for launch vehicles – Typical Performance Values -Mission design – Structural design aspects during launch – role of launch environment on launch vehicle integrity.\n<\/p>\n

Unit II<\/h4>\n

SELECTION OF ROCKET PROPULSION SYSTEMS
\nAscent flight mechanics – Launch vehicle selection process – Criteria for Selection for different missions – selection of subsystems – types of staging – Interfaces – selection and criteria for stages and their role in launch vehicle configuration design.\n<\/p>\n

Unit III<\/h4>\n

Download the iStudy App for all syllabus and other updates.<\/a>
\"Get<\/a><\/h4>\n

Unit IV<\/h4>\n

THRUST VECTOR CONTROL
\nTVC Mechanisms with a Single Nozzle – TVC with Multiple Thrust Chambers or Nozzles – Testing – Integration with Vehicle – SITVC method – other jet control methods – exhaust plume problems in space environment\n<\/p>\n

Unit V<\/h4>\n

NOSE CONE CONFIGURATION
\nAerodynamic aspects on the selection of nose shape of a launch vehicle – design factors in the finalization of nose configuration with respect to payload – nose cone thermal protection system -separation of fairings – payload injection mechanism\n<\/p>\n

Course Outcomes:<\/h4>\n

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