Lectures related to Rocket engine nozzle

Covers the fundamentals of liquid bi-propellant propulsion systems and their operational architectures.

Covers the design process for a 200 N bi-propellant thruster, focusing on key parameters and methodologies for effective performance.

Explores the principles of Inertial and Magnetic Fusion, discussing energy balance, challenges, and progress towards burning plasma.

Explores engine thrust analysis using Munson EX 5.15 and the first law of thermodynamics.

By the EPFL Rocket Team explores the control of rocket descent for a safe vertical landing.