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.

Notes and material for ME 461/561 Gas Dynamics course

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.

An object-oriented Python 3 GUI and API for single- and multi-element Bézier-parametrized airfoil design, analysis, and optimization

Notes and material for Rocket Propulsion course

2D two-fluid Matlab code for divergent Magnetic Nozzles

A comprehensive solution for designing and optimizing student-built liquid rocket engines.

A comprehensive repository for designing, simulating, and analyzing thermal protection systems and heat shielding for spacecraft and rockets.

🚀 Rocket calculations in Python using Cantera

Advanced Kinetic Iterative pLasma Expansion Solver 2D

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

The Future of Space Travel: Quantum-Powered, AI-Driven Propulsion

Simulation of a rocket undergoing pogo oscillation effect

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.

Course notes for ME 3276 Propulsion taught at UConn

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.