propulsion
There are 38 repositories under propulsion topic.
jet/FsKafka
Minimal F# wrappers for Confluent.Kafka+librdkafka.redist 1.x
jet/dotnet-templates
Example app and service templates `dotnet new -i Equinox.Templates; dotnet new eqx*/pro*` https://github.com/jet/equinox https://github.com/jet/FsCodec
alopezrivera/huracan
Open source, 0-dimensional, object-oriented airbreathing engine modelling package for preliminary analysis and design of airbreathing engines, divulgation and educational purposes.
kyleniemeyer/gas-dynamics-notes
Notes and material for ME 461/561 Gas Dynamics course
abdolrezat/TURBN-Turbine-Design
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!
jonnyhyman/PyBurn
Hybrid Rocket Propulsion Model [Python]
usuaero/PyProp
The ultimate electric propulsion modeling and optimization module.
kyleniemeyer/rocket-propulsion
Notes and material for Rocket Propulsion course
ep2lab/dimagno
2D two-fluid Matlab code for divergent Magnetic Nozzles
mlau154/pymead
An object-oriented Python 3 GUI and API for single- and multi-element Bézier-parametrized airfoil design, analysis, and optimization
djangovanderplas/LiquidEngineSizingTool
A comprehensive solution for designing and optimizing student-built liquid rocket engines.
ep2lab/akiles
Advanced Kinetic Iterative pLasma Expansion Solver 2D
kyleniemeyer/RoCt
🚀 Rocket calculations in Python using Cantera
KOSASIH/thermal-protection-system
A comprehensive repository for designing, simulating, and analyzing thermal protection systems and heat shielding for spacecraft and rockets.
anant347/Ion-Propulsion-system-comparison-tool
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.
bryanwweber/propulsion-notes
Course notes for ME 3276 Propulsion taught at UConn
Carmeisel101/RealEngineCycle_TurboProp
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
gottardini/liquidrocket
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.
KOSASIH/FTL-Nexus
The Future of Space Travel: Quantum-Powered, AI-Driven Propulsion
Mirlenko/Propulsion_Plants_Maintenance_Prediction
Gas Turbine and Compressor Decay State Coefficients Prediction
Rishit-katiyar/Rocket_Pogo_Effect_Simulation
Simulation of a rocket undergoing pogo oscillation effect
Spetnik/serverless-blockchain-rocket
Blockchain-powered crypto-propulsion system for interplanetary exploration
trenton-charlson/engine-dev
liquid rocket engine design, development, and sizing code
luihabl/gitgm
Gridded ion thruster global model
mighty-sparrow/lars
Launch And Recovery System for a water rocket.
VictorAlulema/UAVs-propulsion-systems-Database
Database of propulsion system components for electric and fuel powered UAVs
zer0Kerbal/ElephantEngine
A 75% 'Mammoth', consisting of 3 Vectors in a 3.75m base. Mode switching for Elephant-Plume effects! For Kerbal Space Program.
Beach-Launch-Team-CSULB/Igniter-Testing
Contains code used to record thermocouple and pressure transducer data for igniter testing.
yiqiangjizhang/Turbofan-Parametric-Study
The project aims to study the parametrical parameters of a two-spool turbofan with convergent nozzles
sharkman5046/Supersonic-Nozzle-Design
Set of Python classes that allows computations for contours of supersonic nozzles
arda-guler/NuclearPhotonicRocket
Basic nuclear photonic rocket design study
Beach-Launch-Team-CSULB/JAWS-1
Development of BLT's first regen engine
bxrne/launchrail
(WIP!) Experimenting with the idea of creating a 6-DOF High Power Rocketry simulator.
l-jordan/Propeller-BEM
Simple blade element propeller momentum theory analysis to analyse speeds of aircraft in forward flight.
tar7operator/Pinaka
Rocketry Team