What is it about?
Preliminary insight on a Liquid Propellant Combustion Chamber.
Featured Image
Why is it important?
Its brings a more useful way to specify the geometry of Combustion Chamber.
Perspectives
Read the Original
This page is a summary of: A parametric model for thrust chamber preliminary design, July 2016, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2016-4936.
You can read the full text:
Contributors
The following have contributed to this page