Aircraft and Rocket Propulsion
This course is an introduction to the design and performance of airbreathing and rocket engines and the physical parameters used to characterize propulsion system performance.
Topics Include
- Gas dynamics of nozzles and inlets
- Cycle analysis of ramjets, turbojets, turbofans, and turboprops
- Component matching and the compressor map
- Introduction to liquid and solid propellant rockets
- Multistage rockets
- Hybrid rockets
- Thermodynamics of reacting gases
Course Page
Price
$4,056.00
Subject to change
Delivery
Online, instructor-led
Level
Introductory
Commitment
10 weeks, 5-15 hrs/week
School
Stanford School of Engineering
Language
English