Liquid Rocket Engines for
Spacecraft Pressure-Fed Propulsion Systems
Dates/Course Number
ASTE 0525 - 06
3 Saturdays
May 31, 2025
June 7, 2025
June 14, 2025
Time
9:00am - 5:00pm pacific time
Cost
$3850 - On-Campus
$3850 - Online-Interactive
$3080- Boeing On-Campus
$3080 - Boeing Online-Interactive
Registration closes 05/23.
What You Will Learn:
Pressure-fed liquid propellant rocket engines are and will continue to be used in satellite propulsion systems. Understanding of basic principles of rocketry, thermo-chemistry, fluid mechanics, and heat transfer and their application to design, analysis, and testing of these thrusters is the key not only to satellite nominal operations but also to recovering from some off-nominal situations. In addition to accomplishing these objectives, this course will enable the participants to better converse with spacecraft subsystem specialists, mission planners, designers, and operators.
Extensive set of course notes developed by the instructor provide concise reference on pressure-fed, monopropellant, bipropellant, dual mode, and secondary combustion augmented thrusters. The course covers:
- Basics of Rocketry
- Thrust Chamber Assembly (TCA) --- Valves, Injectors, Chamber, and Nozzle
- Thrust Chamber Materials and Coatings
- Thrust Chamber Cooling Techniques
- Thermal Modeling of Fuel Film-cooled Thrusters
- Combustion Instability
- Flight operations
- Hot-fire Testing and Data Analysis
- Anomaly Investigations and Resolutions