LESSON PLAN_Rockets and Missiles
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Page 1 of 2 LESSON PLAN 1. Course Title : Rockets & Missiles 5. Semester : VII 2. Course Code : AE 404 6. Academic Year : 2015-16 3. Course Faculty : Mohammad Fazlur Rahman 7. Department : Aerospace Engg. 4. Theory/Practical : Theory 8. No. of Credits : 3 9. Course Learning Objectives: To introduce basic concepts of design and trajectory estimation of rocket and missiles. 10. Course pre-requisites: Basics of Aircraft engines, Projectile motion, Aerodynamic Forces, Physics, Chemistry, Mathematics 11. Schedule of teaching and learning Sl.No. Period Topic Mode of Teaching Aids Reference/ delivery Source 1. All All Lecture Black Board /PPT Books 12. Course material and References 1. Cornelisse, J.W., “Rocket Propulsion and Space Dynamics”, J.W. Freeman & Co., Ltd, London, 1979 2. Sutton, G.P., “Rocket Propulsion Elements”, John Wiley & Sons, 2000. 13. Assessment Scheme: i) Periodical tests Continuous Assessment Test-3 ii) Assignment Assignments-3 iii) Classroom objective type tests Classroom tests-3 Date: July 19, 2015 Course Faculty Head of Department
description
This document presents the lesson plan to handle the course named "Rockets & Missiles" in the B. S. Abdur Rahman University.The syllabus says that last unit must take 6 hours which I have cut short to 4 hours and given two extra hours to multi staging topics to handle the numerical problems.
Transcript of LESSON PLAN_Rockets and Missiles
Page 1 of 2
LESSON PLAN
1. Course Title : Rockets & Missiles 5. Semester : VII
2. Course Code : AE 404 6. Academic Year : 2015-16
3. Course Faculty : Mohammad Fazlur Rahman 7. Department : Aerospace Engg.
4. Theory/Practical : Theory 8. No. of Credits : 3
9. Course Learning Objectives:
To introduce basic concepts of design and trajectory estimation of rocket and missiles.
10. Course pre-requisites:
Basics of Aircraft engines, Projectile motion, Aerodynamic Forces, Physics, Chemistry, Mathematics
11. Schedule of teaching and learning
Sl.No. Period Topic Mode of Teaching Aids Reference/
delivery Source
1. All All Lecture Black Board /PPT Books
12. Course material and References
1. Cornelisse, J.W., “Rocket Propulsion and Space Dynamics”, J.W. Freeman & Co., Ltd, London, 1979
2. Sutton, G.P., “Rocket Propulsion Elements”, John Wiley & Sons, 2000.
13. Assessment Scheme:
i) Periodical tests
Continuous Assessment Test-3
ii) Assignment
Assignments-3
iii) Classroom objective type tests
Classroom tests-3
Date: July 19, 2015 Course Faculty
Head of Department
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Lesson Plan (AE 404 Rockets and Missiles)
UNIT No Topics to be covered Duration
in Periods
Teaching method
BB/PP/Video
Module I
Basics of aircraft propulsion and non-air breathing engines.
1 BB/PPT
Solid rockets and solid rockets propellants and its types 3 BB/PPT
Combustion mechanism of propellants 1 BB/PPT
Liquid rocket and propellants and their classification 2 BB/PPT
Feedlines and liquid rocket thrust chambers 2 BB/PPT
Rocket ignition and igniters 1 BB/PPT
Total Periods 10
Module II
Airframe components of Rockets and Missiles 1 BB/PPT
Aerodynamics forces on the missiles, slender body aerodynamics
4 BB/PPT
Lateral forces and moments on rockets 2 BB/PPT
Classification of missiles, drag estimation, rocket dispersion
3 BB/PPT
Total Periods 10
Module III
One dimensional and two-dimensional rocket motions in free space and homogeneous gravitational fields
3 BB/PPT
Rocket Trajectory 2 BB/PPT
Range and Altitude 2 BB/PPT
Burn out velocity and altitude 2 BB/PPT
Culmination time and altitude 1 BB/PPT
Total Periods 10
Module IV
Multistage introduction and launch vehicles and missiles, 2 BB/PPT/VID
Stage optimization 2 BB/PPT
stage separation technique, dynamics & characteristics 2 BB/PPT
Thrust vector control 2 BB/PPT/VID
Numerical on stage separation and multistaging 3 BB/PPT
Total Periods 11
Module V
Material properties for rockets and missiles 1 BB/PPT
Material for airframe components and parts 1 BB/PPT
Material for TVC 1 BB/PPT
Adverse conditions and rocket materials for this 1
Total Periods 4
TOTAL PERIODS 45 Hours
