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

Propellant Evaluation Program for z/OS

LETALIS: Liquid Propellant Rocket Engine thermal analysis and cooling system design.

A tool for preliminary design and regenerative cooling modelling of liquid propellant rocket engines

🚀 Professional rocket engine simulation & 6-DOF flight analysis platform. NASA CEA validated thermochemistry, real-time performance calculations, Monte Carlo dispersion analysis.

Rocket engine thrust chamber contour model.

A Rest API that serves informations about orbital rocket engines

Node based Express server that will control, gather, & send relevant information on a pressure fed liquid rocket engine.

Conceptual design and analysis of a liquid-propellant rocket engine for orbital launch vehicles. Presents key specs (chamber pressure, nozzle expansion, thrust-to-weight), propellant/material selection (LOX/RP-1 & LOX/LH₂), cycle considerations, and computational workflows for engine sizing, sweeps and trade-off studies.

InjectorWIZARD

Simulator for rocket engine, powered by gas expansion.

Physics-Informed LSTM for rocket engine RUL prediction — Chaboche/GRCop-84, NASA C-MAPSS validation

This repository contains a small, focused **AI-assisted health monitoring** demo for a **liquid-propellant rocket engine**.

Explore your favorite rocket engines and compare them.

This project demonstrates how AI/ML can be applied to monitor the health of a liquid-propellant rocket engine using **synthetic telemetry data**.

Luna Executor is a robust tool for executing custom scripts in Roblox, enhancing your gameplay with unique features. Join our community on Discord to share insights and access exclusive tools, all while enjoying a user-friendly experience. 🐙💻

Information for the 2026 hybrid rocket engine final year project.

ENMA: Empirical Nozzle optimization & Mach distribution Analysis for liquid propellant rocket engines.

Open-source LOX–methane rocket engine cycle analysis framework: gas generator, oxidizer-rich staged, and full-flow staged combustion comparison with regenerative cooling, MCDA trade study, and Indian mission case.

CT Scan Analyzer for Rocket Engine