Preliminary design of a liquid rocket engine for in-space applications using semi-cryogenic propellants (LOX-RP1), responsible for the design and losses of the injection plate and of the nozzle
-
Updated
Mar 21, 2026 - MATLAB
Preliminary design of a liquid rocket engine for in-space applications using semi-cryogenic propellants (LOX-RP1), responsible for the design and losses of the injection plate and of the nozzle
Add a description, image, and links to the injection-device topic page so that developers can more easily learn about it.
To associate your repository with the injection-device topic, visit your repo's landing page and select "manage topics."