propulsion

Minimal F# wrappers for Confluent.Kafka+librdkafka.redist 1.x

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!

Hybrid Rocket Propulsion Model [Python]

The ultimate electric propulsion modeling and optimization module.

Notes and material for ME 461/561 Gas Dynamics course

🚀 Rocket calculations in Python using Cantera

Advanced Kinetic Iterative pLasma Expansion Solver 2D

Predictive energy management for hybrid-electric aircraft with parallel propulsion system.

2D two-fluid Matlab code for divergent Magnetic Nozzles

Notes and material for Rocket Propulsion course

Course notes for ME 3276 Propulsion taught at UConn

Blockchain-powered crypto-propulsion system for interplanetary exploration

Repository for pymead, an object-oriented Python 3 package for single- and multi-element Bézier-parametrized airfoil design, analysis, and optimization

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.

A 75% 'Mammoth', consisting of 3 Vectors in a 3.75m base. Mode switching for Elephant-Plume effects! For Kerbal Space Program.

Launch And Recovery System for a water rocket.

Database of propulsion system components for electric and fuel powered UAVs

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.