Free Course Image Aerospace Engineering

Free online course Aerospace Engineering

Duration of the online course: 17 hours and 32 minutes

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Build in-demand aerospace skills with a free online course on rocket dynamics, orbits, nozzles, and propulsion—learn fast and earn a certificate-ready foundation.

In this free course, learn about

  • How rocket dynamics differ from cars/projectiles; motion in space basics
  • Impulse–momentum and force relationships relevant to spaceflight
  • Rotating frames, orbital velocities, and circular Earth orbit speed
  • Velocity requirements: delta‑V, escape velocity, and GEO altitude
  • Rocket propulsion theory: thrust generation and propulsion efficiency
  • Tsiolkovsky rocket equation, payload fraction tradeoffs, and staging benefits
  • Nozzle theory: throat choking, optimal expansion, and specific impulse units
  • Nozzle geometries: conical vs bell, divergence loss, and typical divergence angles
  • Unconventional altitude-compensating nozzle concepts (e.g., dual-mode step nozzle)
  • Characteristic velocity (c*) and thrust coefficient; what improves them
  • Chemical propellant selection criteria: mixture ratio, fuel-rich choices, performance
  • Performance prediction: chamber pressure effects, dissociation, equilibrium vs frozen flow
  • Solid rocket fundamentals: composite composition, burning rate, and gas generation rate
  • Why double-base propellants suit tactical missiles vs composite propellants

About the free online course

Step into the engineering behind rockets and spacecraft and learn to reason about flight where everyday intuition stops working. This free online course introduces the physical principles that govern motion beyond the atmosphere, helping you connect forces, momentum, and reference frames to the realities of spaceflight. You will gain a solid foundation in how rockets differ from cars, aircraft, or simple projectiles, and why space missions are driven by velocity requirements, orbital mechanics, and careful propulsion design.

You will work through the core ideas that shape modern aerospace engineering, from motion in space and rotational frames of reference to the practical meaning of orbital speed, circular orbits, and geostationary altitude. Instead of treating these as isolated facts, the course builds engineering judgment: how to estimate what it takes to reach orbit, when escape velocity matters, and how mission delta V influences the entire vehicle architecture. This context is essential for anyone considering careers in aerospace, mechanical systems, or adjacent fields that value rigorous modeling and systems thinking.

A major focus is rocket propulsion, including the rocket equation, staging strategies, and propulsion efficiency. You will learn how design tradeoffs affect payload fraction, why upper stages are so influential, and what performance constraints appear at liftoff compared with high-altitude flight. The course then connects theory to hardware through nozzle concepts: throat conditions, expansion for maximum thrust, characteristic velocity, thrust coefficient, divergence losses, and common geometries such as conical and bell nozzles, along with unconventional designs that adapt across altitude.

Finally, you will explore how engineers choose propellants and predict performance, including mixture ratio effects, chamber pressure influences on combustion chemistry and dissociation, and how equilibrium or frozen-flow assumptions change results. The course also introduces solid rocket fundamentals, typical composite propellant composition, gas generation from burning surfaces, and why certain propellant families are preferred in specific mission types. With targeted exercises throughout, you will finish with a practical, confidence-building understanding of how rockets are analyzed and why real-world propulsion decisions look the way they do.

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-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-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-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:

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17 hours and 32 minutes of online video course

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Digital certificate of course completion (Free)

Icon for exercises to practice what you've learned

Exercises to train your knowledge

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100% free, from content to certificate

Why is rocket motion different from the motion of a car or a projectile?

A rocket accelerates by ejecting mass, so its mass changes continuously and it can generate thrust in space without air or ground contact.

What is the approximate escape velocity from Earth's surface?

Earth's escape velocity is approximately 11.2 km/s, ignoring atmospheric drag and Earth's rotation.

What condition gives maximum thrust in a rocket nozzle?

Maximum thrust occurs when the nozzle exit pressure matches the surrounding ambient pressure.

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Course comments: Aerospace Engineering

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Sanket S Anchekar

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