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4 search results found

Cooling system modelling for liquid rocket engines.

Rocket Solver ⭐ 7

Python package that helps engineers design rockets and rocket engines precisely and efficiently

QC report generator for Hi-C pairs file

Axisymmetric Method Of Characteristics Nozzle Designer With Gui ⭐ 5

This programme was developed in conjunction with a paper on the matter named "A Detailed Presentation and Implementation Procedure of Axisymmetric Method of Characteristics for Rocket Nozzle Design". Developed by Kyril Palaveev and Dr. Torsten Schenkel, the software is meant to allow users to easily compute axisymmetric rocket nozzles utilizing the iterative Axisymmetric Method of Characteristics (MOC) procedure. The methodology is thoroughly described in the uploaded paper (.pdf file)

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1-4 of 4 search results

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