This is an open-source application for ship machinery configuration.
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Updated
Jan 6, 2023 - JavaScript
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
The project aims to study the parametrical parameters of a two-spool turbofan with convergent nozzles
Contains code used to record thermocouple and pressure transducer data for igniter testing.
Gridded ion thruster global model
Launch And Recovery System for a water rocket.
A 75% 'Mammoth', consisting of 3 Vectors in a 3.75m base. Mode switching for Elephant-Plume effects! For Kerbal Space Program.
Database of propulsion system components for electric and fuel powered UAVs
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.
Simulation of a rocket undergoing pogo oscillation effect
Blockchain-powered crypto-propulsion system for interplanetary exploration
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
liquid rocket engine design, development, and sizing code
Gas Turbine and Compressor Decay State Coefficients Prediction
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.
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