Parametric luquid engine design tool , requirements become inputs and then they become constraints. They get sized and the output is a 3D-printable engine
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Updated
Oct 25, 2026 - Python
Parametric luquid engine design tool , requirements become inputs and then they become constraints. They get sized and the output is a 3D-printable engine
Liquid bipropellant engine design from requirements: CEA thermochemistry, Rao bell contour, losses, Bartz heat flux, validated against RS-25, RL10B-2 and Merlin 1D, with a Streamlit app.
火箭发动机试车数据离线解析、校准与分析:推力/燃烧室压力/温度,TR_F/TR_P/TR_T、CSV/TSV/XLSX,实验与理论曲线对齐、FFT,导出 CSV/PNG、TXT/JSON 报告及 ENG(需满足输入条件)。 | Offline rocket motor/engine test data analysis: thrust/chamber pressure/temperature; TR_F/TR_P/TR_T, CSV/TSV/XLSX import; calibration, experiment/theory alignment, FFT; CSV/PNG, TXT/JSON reports and ENG export with required inputs.
LGJ Propulsion Analysis — liquid rocket thrust chamber design, performance, and thermal analysis
Verifiable AI agent for engine test data: every number in the report traces back to a reproducible computation.
🚀 Professional rocket engine simulation & 6-DOF flight analysis platform. NASA CEA validated thermochemistry, real-time performance calculations, Monte Carlo dispersion analysis.
Deep-RL control of liquid rocket engines, built on DLR's LUMEN Control Challenge: literature review, domain primer, a labelled LUMEN-like surrogate with PI, PPO and SAC baselines, and an in-browser Engine Lab with an animated test stand
Rocket engine thrust chamber contour model.
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.
Physics-Informed LSTM for rocket engine RUL prediction — Chaboche/GRCop-84, NASA C-MAPSS validation
CT Scan Analyzer for Rocket Engine
This repository contains a small, focused **AI-assisted health monitoring** demo for a **liquid-propellant rocket engine**.
This project demonstrates how AI/ML can be applied to monitor the health of a liquid-propellant rocket engine using **synthetic telemetry data**.
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.
Simulator for rocket engine, powered by gas expansion.
A comprehensive solution for designing and optimizing student-built liquid rocket engines.
LETALIS: Liquid Propellant Rocket Engine thermal analysis and cooling system design.
ENMA: Empirical Nozzle optimization & Mach distribution Analysis for liquid propellant rocket engines.
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