In this article, we are glad to provide the syllabus of the code AS3611 of Anna University awarding the B.E Aerospace Engineering Syllabus based on regulation 2021. Let’s what we have here.
We tried our best to provide the detailed syllabus unit-wise for the subject code AS3611 – Space Launch Vehicle Design Project Semester VI. We also include the required textbooks and references from the expert faculty regarding the syllabus. Along with it assists the students to become more aware of the topics. And can easily make preparation strategies as per the syllabus to make your move for examinations. Hope this information is useful. Comment below if you need anything relevant to the syllabus. We’ll try to answer your questions. Don’t forget to share with your classmates.
If you want to know more about the B.E Aerospace Engineering Syllabus connected to an affiliated institution’s four-year undergraduate degree program. We provide you with a detailed Year-wise, semester-wise, and Subject-wise syllabus in the following link B.E Aerospace Engineering Syllabus Regulation 2021 Anna University.
Aim Of Concept:
- To make the student work in groups and effectively improve their team work.
- To understand the concepts involved in designing the space launch vehicle.
- To learn the conceptual stage of a spacecraft design in respect of its stability.
- To Understand the necessary phases in the design process and produce the required outcomes of each phase.
AS3611 – Space Launch Vehicle Design Project Syllabus
Tasks:
- Classification of rocketry & launch vehicles.
- Current & future launch vehicles, Orbit/trajectory requirements and missions.
- Rocket propulsion: generation of thrust, the rocket equation. Specific impulse, types of engines, Launch vehicle parameters & performance.
- Staging, Structure & propulsion design trades.
- Powered flight. Gravity loss, Ascent through the atmosphere, drag loss, Vehicle coordinates, moving coordinate systems, The local horizon frames. Motion of the launch site, Ascent trajectories, The gravity-turn trajectory, Numerical calculation of trajectories.
- Application of software in trajectory calculation, Optimization principles, Introduction to GPOPS2 program & application to launch optimization, Structures: tanks, inter-tank & interstage structure, thrust structure, separation systems.
- Δv & initial sizing, inboard profile & layout, Engine selection, Preliminary mass estimation.
- Loads from ground winds, loads during flight: thrust, aero, & inertial forces, Trimmed flight, Max-q, Calculation of internal forces, moments, shears.
- Calculation of stresses due to external loads, internal pressurization, Tank & inter-stage structural design, Vibration, shock, acoustic, and thermal effects.
- VS&A, thermal, concluded Guidance, stability & control.
- Structural flexibility effects, Instabilities, Manufacturing, Launch pad & facilities.
- Ground testing, Safety & flight termination systems.
References:
- Griffin and French, “Space Vehicle Design”, AIAA, 2004, ISBN 1563475391.
- Meyer R., “Elements of Space Technology”, Academic Press, 1999, ISBN 0124929400
- Sforza, “Manned Spacecraft Design Principles”, Elsevier, 2016, ISBN 9780128044254
- Walter U., “Astronautics”, WILEY-VCH, 2008, ISBN 9783527406852
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