Rockets and Missiles detailed syllabus for Aeronautical Engineering (AERO), R18 regulation has been taken from the JNTUHs official website and presented for the students of B.Tech Aeronautical Engineering branch affiliated to JNTUH course structure. For Course Code, Course Titles, Theory Lectures, Tutorial, Practical/Drawing, Credits, and other information do visit full semester subjects post given below. The syllabus PDF files can also be downloaded from the universities official website.
For all the other AERO 4th Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH scheme, visit Aeronautical Engineering 4th Year 1st Sem R18 Scheme.
For all the (Professional Elective-2) subjects refer to Professional Elective-2 Scheme. The detail syllabus for rockets and missiles is as follows.
Course Objective:
- To compute and analyze the various forces and moments acting on a rocket
- To formulate the equations of motions for flight and separation phases
- To understand the combustion and propulsion systems in rocket
- To select suitable materials for the rockets and missiles
- To understand the design, performance and testing aspects
Course Outcome:
For the complete syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier.
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Unit – I
Rocket Dynamics: Classification of launch vehicles and missiles – Rocket systems – Airframe components – Forces and moments acting on a rocket – Propulsion, aerodynamics, gravity – inertial and non-inertial frames – coordinate transformation – Equations of motion for three-dimensional motion through atmosphere and vacuum, earths atmosphere, numerical problems
Unit – II
Solid Propulsion and Pyrotechnics: Solid propellant rockets – classification, components and their design considerations, propellant grain design – grain mechanical properties, ballistics and burn rate design issues – igniter design – types of nozzles and thrust vector control, pyrotechnic devices and systems-classification, mechanisms and application of pyrotechnic devices in rockets and missiles. Design problems in rocket systems.
Unit – III
For the complete syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier..
Unit – IV
Multi-Staging of Rocket and Separation Dynamics: Navigation and guidance systems in rockets and missiles – aerodynamic control systems of missiles- multi-staging of rockets – vehicle optimization techniques -stage separation system – dynamics, separation techniques – rocket flight dispersion, numerical problems.
Unit – V
Design, Materials and Testing of Rockets: Design requirements and selection, performance evaluation and assessment, space environment on the selection of materials for rockets and spacecraft, material selection for specific requirements, advance materials-super alloys and composite materials. Qualification of rocket and missile systems, types of testing and evaluation of design and function.
Text Books:
For the complete syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier..
Reference Books:
- Ronald Humble, Henry and Larson.Space Propulsion Analysis and Design. Mc Graw-Hill. 1995
- George M. Siouris, Missile Guidance and Control Systems, Springer-Verlag New York, 2000.
For detail syllabus of all other subjects of B.Tech Aeronautical Engineering 4th Year 1st Sem , visit AERO 4th Year 1st Sem syllabus subjects.
For B.Tech Aeronautical Engineering (AERO) 4th Year results, visit JNTUH B.Tech Aeronautical Engineering semester results direct link.