There are 5 repositories under propulsion topic.
Example app and service templates `dotnet new -i Equinox.Templates; dotnet new eqx*/pro*` https://github.com/jet/equinox https://github.com/jet/FsCodec
Open source, 0-dimensional, object-oriented airbreathing engine modelling package for preliminary analysis and design of airbreathing engines, divulgation and educational purposes.
A MATLAB GUI for estimating some properties of turbines, the code is mainly based on Mattingly's "Elements of Propulsion". This repository is made for educational purposes, it does solve the problems in the book so it would be a useful resource for students. See the interface screenshots or just run the code, it's pre-loaded with examples!
Notes and material for ME 461/561 Gas Dynamics course
Hybrid Rocket Propulsion Model [Python]
A comprehensive solution for designing and optimizing student-built liquid rocket engines.
🚀 Rocket calculations in Python using Cantera
Course notes for ME 3276 Propulsion taught at UConn
A python GUI app that helps a user to compare various ion engines by plotting a 'Total spacecraft mass by thrust' graph and generating a log that includes various calculated parameters.
This is a full cycle code for the PT6A-114 engine. The code was developed for AERO 417 Aerospace Propulsion. In this repository, you will find the code for the engine, as well as the basic engine specs and code results
Source code of a university project. It is a liquid rocket engine designer that calculates a multitude of geometrical and thermodynamical variables with given performance constraints.
Gas Turbine and Compressor Decay State Coefficients Prediction
Blockchain-powered crypto-propulsion system for interplanetary exploration
liquid rocket engine design, development, and sizing code
Launch And Recovery System for a water rocket.
Database of propulsion system components for electric and fuel powered UAVs
A 75% 'Mammoth', consisting of 3 Vectors in a 3.75m base. Mode switching for Elephant-Plume effects! For Kerbal Space Program.
Contains code used to record thermocouple and pressure transducer data for igniter testing.
The project aims to study the parametrical parameters of a two-spool turbofan with convergent nozzles
This is an open-source application for ship machinery configuration.
Set of Python classes that allows computations for contours of supersonic nozzles
Basic nuclear photonic rocket design study