Rocket and Missiles detail syllabus for Aeronautical Engineering (Aero), 2019-20 scheme is taken from AKTU official website and presented for AKTU students. The course code (RAE070), and for exam duration, Teaching Hr/Week, Practical Hr/Week, Total Marks, internal marks, theory marks, and credits do visit complete sem subjects post given below.
For all other aero 7th sem syllabus for b.tech 2019-20 scheme aktu you can visit Aero 7th Sem syllabus for B.Tech 2019-20 Scheme AKTU Subjects. For all other Departmental Elective-3 subjects do refer to Departmental Elective-3. The detail syllabus for rocket and missiles is as follows.
Unit I
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Unit II
Chemical propellants:Propellant formula and mixture ratio, Effects of initial speed of reactants on the adiabatic flame temperature. Calculation of equilibriums compositions, systems containing only hydrogen and oxygen and system containing hydrogen, carbon, oxygen and nitrogen. Applicability of Dalton’s law to chemical rocket motors,
Hybrids and electric propulsion: Applications of hybrid propellants. Electro thermal, electro static and electromagnetic propulsion systems.
Unit III
Solid Propellants:Propellants characteristics, grain and grain configuration. Classifications of grains, fundamental properties of burning grain surface. Basic chemicals of solid propellants and oxidizers, fuels, binders, Propellants burning rate, burning rate modifiers and plasticizers. Manufacturing of solid propellants. Thrust time trace of solid propellants rockets. Strand burner method of temperature measurement and end burning. Elements of combustion instability. Auxiliary uses of solid propellants, gas generators.
Liquid propellants:Propellants characteristics specifications in view economic factors, performance of propellants, common physical hazards. Desirable physical and combustion properties. Various liquid propellants. Propellants feed systems, gas pressure feed system and turbo pump feed system.
Unit IV
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Unit V
Thrust vector controls and Engines controls:Thrust vector control with single nozzle and with multiple thrust chambers or nozzles. Testing of thrust vector control system. Control of engine starting and thrust build ups.
Introduction to Missiles: Classifications of missiles: Guidance phases during flight; Categories of Homing and command guidance. Classification of Missile Guidance laws; modern guidance law Pure Pursuit Guidance Law.Basic Results in Interception and Avoidance
Books and References:
- Barrers, M, Jaumolte, A, De Vaubeke, B, F, and Vandenkerchove, J, Rocket Propulsion, Elsevier Publishing Company 1960,
- Hill, P, G, and Peterson, C, R, Mechanics and Thermodynamics of Propulsion, Addison-Wesely Publishing Company 1965.
- Penner, S, S, Chemistry Problem in Jet Propulsion, Macmillan Company, 1957.
- Koelle, H, H, ( Edr,) Handbook of Astronautically Engineering , McGraw – Hill Book .
- Sulton, G, P, Rocket Propulsion Elements, John Wiley and Sons 1963.
- Zucrow, M, J, Aircraft and Missile Propulsion – Vol, I and II, John Wiley and Sons, 1958.
- Williams, FA, Barrere, M, and Huang, N, C, Fundamental Aspects of Solid Propellant Rockets.
For detail syllabus of all other subjects of B.Tech Aero, 2019-20 regulation do visit Aero 7th Sem syllabus for 2019-20 Regulation.
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