Free Course Image Aerospace Engineering

Free online courseAerospace Engineering

Duration of the online course: 17 hours and 32 minutes

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Explore aerospace engineering fundamentals with NPTEL's free online course. Learn rocket propulsion, orbital dynamics, and more. Perfect for aspiring engineers.

In this free course, learn about

  • Introduction to Spaceflight and Orbital Mechanics
  • Mission Velocity Requirements and Basic Rocket Propulsion
  • Nozzle Theory, Design, and Performance
  • Chemical Propellants and Solid Rocket Motors

Course Description

Discover the fascinating world of aerospace engineering with NPTEL's comprehensive online course. Delve into the dynamics of space motion, beginning with an engaging introduction followed by an in-depth exploration of motion in space and the complexities of rotational frames of reference and orbital velocities. Understand the intricacies of velocity requirements essential for space travel.

The course offers a thorough examination of rocket propulsion theories and mechanics. From the foundational rocket equation to the challenges of rocket staging, each module builds on the previous to provide a cohesive understanding of propulsion. Critical concepts such as propulsion efficiency and nozzle theories are explored through real-world examples, offering practical insights into aerospace engineering challenges.

Understand the factors influencing chemical propellant choices and the roles of characteristic velocity and thrust coefficient in determining rocket performance. Nozzle dynamics are extensively covered, from traditional shapes to unconventional designs, including the conical and bell nozzles, highlighting performance and efficiency considerations.

Uncover the criteria for selecting chemical and fuel-rich propellants and engage with performance prediction analyses. Discussion on shifting equilibrium and frozen flow in nozzles provides insights into advanced propulsion systems. Explore the basics of solid propellant rockets, gaining an understanding of propellant types and their applications in modern aerospace contexts.

This online course is suited to those interested in deepening their knowledge in engineering and mechanics. It offers a unique opportunity to learn at your own pace while gaining substantial skills in aerospace engineering principles.

Course content

  • Video class: Mod-01 Lec-01 Introduction 57m
  • Exercise: Why does rocket dynamics differ fundamentally from that of a car or a projectile fired from a gun?
  • Video class: Mod-01 Lec-02 Motion in Space 45m
  • Exercise: Impulse and Force Relationship
  • Video class: Mod-01 Lec-03 Rotational Frame of Reference and Orbital Velocities 41m
  • Exercise: Orbital velocity for a circular Earth orbit
  • Video class: Mod-01 Lec-04 Velocity Requirements 52m
  • Exercise: Height of a Geostationary Orbit (in km)
  • Video class: Mod-01 Lec-05 Theory of Rocket Propulsion 50m
  • Exercise: What is the approximate escape velocity from Earth’s surface?
  • Video class: Mod-01 Lec-06 Rocket Equation and Staging of Rockets 55m
  • Exercise: For a fixed mission delta V and structural mass, which change increases the payload mass fraction in the ideal rocket equation?
  • Video class: Mod-01 Lec-07 Review of Rocket Principles: Propulsion Efficiency 59m
  • Exercise: Booster-stage performance: which parameter matters most at liftoff when propellant mass fraction is small?
  • Video class: Mod-01 Lec-08 Examples Illustrating Theory of Rocket Propulsion and Introduction to Nozzles 54m
  • Exercise: Why do upper stages contribute more delta V in a multistage rocket?
  • Video class: Mod-01 Lec-09 Theory of Nozzles 51m
  • Exercise: In SI units, what is the correct unit for specific impulse in rocket propulsion
  • Video class: Mod-01 Lec-10 Nozzles Shapes 52m
  • Exercise: Condition at the throat for maximum acceleration in a convergent-divergent nozzle
  • Video class: Mod-01 Lec-12 Characteristic Velocity and Thrust Coefficient 54m
  • Exercise: Nozzle expansion condition for maximum thrust
  • Video class: Mod-01 Lec-13 Divergence Loss in Conical Nozzles and the Bell Nozzle 50m
  • Exercise: What semi divergence angle is typically chosen for a conical rocket nozzle to balance thrust loss and nozzle length?
  • Video class: Mod-01 Lec-14 Unconventional Nozzles and Problems in Nozzles 54m
  • Exercise: Which nozzle concept provides two operating modes via a step, enabling separation at low altitude and reattachment at high altitude?
  • Video class: Mod-01 Lec-17 Performance Prediction Analysis 57m
  • Exercise: Effect of chamber pressure on dissociation and properties in H2 O2 rocket combustion
  • Video class: Mod-01 Lec-19 Shifting Equilibrium and Frozen Flow in Nozzles 52m
  • Exercise: Impact of chamber pressure on dissociation and performance
  • Video class: Mod-01 Lec-15 Criterion for Choice of Chemical Propellants 53m
  • Exercise: Which combination best improves characteristic velocity C star in a chemical rocket
  • Video class: Mod-01 Lec-16 Choice of Fuel-Rich Propellants 56m
  • Exercise: Mixture ratio for maximizing c star in chemical rockets
  • Video class: Mod-01 Lec-20 Factors Influencing Choice of Chemical Propellants 51m
  • Exercise: Typical composition of a composite solid propellant
  • Video class: Mod-01 Lec-22 Introduction to Solid Propellant Rockets 52m
  • Exercise: For a solid propellant grain, which relation gives the mass generation rate of gas from the burning surface
  • Video class: Mod-01 Lec-24 Solid Rockets – Propellants 48m
  • Exercise: Why are homogeneous (double‑base) propellants preferred in tactical missiles over composite propellants?

This free course includes:

17 hours and 32 minutes of online video course

Digital certificate of course completion (Free)

Exercises to train your knowledge

100% free, from content to certificate

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