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.


This three-day course provides an overview of the fundamental concepts and technologies of modern satellite liquid propellant rocket engines. The course will concentrate scientific and engineering foundations of pressure - fed, monopropellant, bipropellant, dual mode, and secondary combustion augmented thrusters for satellite orbit-raising and station-keeping operations.
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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

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Custom Programs

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Published on July 11th, 2017Last updated on May 6th, 2025