Fiche personnelle: Daniele Pavarin

L'obbiettivo del corso è fornire i fondamenti per poter comprendere le problematiche di base inerenti il dimensionamento di un apparato propulsivo e/o la sua integrazione nell'ambito di un sistema spaziale.

Catégorie DEPARTMENT OF INDUSTRIAL ENGINEERING / Corsi anni accademici passati / A.A. 2023 - 2024 / Corsi di laurea magistrale / IN0526 - INGEGNERIA AEROSPAZIALE

General introduction about rockets, rocket performance parameters, TSIOLKOVSKY’s equation and its implications, general equation of a vehicle propelled by a rocket system, generalized one-dimensional gasdynamics, one-dimensional isoentropic flow through a convergent-divergent nozzle, Fanno’s flow, Rayleight’s flow, introduction to gas behavior in high temperature conditions, equilibrium and non-equilibrium conditions, fundamentals of thermochemistry, real nozzle behavior. Solid Rockets: general overview of solid rockets, general equations, regression rate low and parameters of influence, propellants, ignition. Liquid Rockets: general overview of liquid rockets, general equations, injection, pressurization systems.

Catégorie DEPARTMENT OF INDUSTRIAL ENGINEERING / Corsi anni accademici passati / A.A. 2024 - 2025 / Corsi di laurea magistrale / IN2807 - AEROSPACE ENGINEERING