Repo for PSAS' liquid propellant engine (LPE) designs (starting with 2015 liquid engine ME capstone and continuing into LV4)

Pintle injector design for all PSAS liquid propellant engines

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

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

Pyskyfire is a simulation framework for regeneratively cooled, liquid propellant rocket engines

Propellant Tank Design for Liquid Propellant Rocket Engines

Internship on Transient Simulation of the Liquid Propellant Rocket Engine at TUM, 10 weeks internship with own models and coding. Based on the report by Gauthier JARY, student at ENSTA Paris.

liquid propellant rocket engine combustion, kerosene_n2o Cantera and Nasa CEA

Repository for the propellant feed team of the Mu engine, APL's first liquid propellant engine.

Repository for the nozzle team of the Mu engine, APL's first liquid propellant engine.

Liquid Propellant Rocket Engine

The SpaceX Raptor BFR is a full-flow, staged-combustion, methane-fueled rocket engine. The propellant used in this engine is cryogenic liquid oxygen and liquid methane. SpaceX is using this engine for the development of Starship, which is a fully reusable system designed to transport crew and cargo to Earth orbit, the Moon, or potentially Mars. Orbital flight has not been implemented yet but is targeted to happen in 2020.

This script is to be used to develop a small liquid bi-propellant rocket engine. It has been tested to be operational for the design of a 150 [lbf] liquid rocket engine using nitrous oxide and isopropanol as the propellants.

RocketSizer is an interactive Python application that allows you to: - Size a liquid propellant rocket engine based on input parameters - Visualize the engine geometry (chamber, convergent, throat, divergent) - Estimate production costs based on mass and complexity

These documents were created as part of the submission of an undergraduate thesis to the Oregon State University Honors College. They detail the design of a Rapid Prototyping Test Stand (RPTS) designed to quicken the development of an electric propellant feed pump for a bi-propellant liquid engine rocket for the HALE student rocketry team.

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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.

Calculation of parameters of combustion products of a liquid propellant rocket engine

Senior Design Project : Investigation of Gas Generators in Liquid Propellant Rocket Engines

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

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

All testing data from ICLR's 2023 liquid bi-propellant engine tests

Repository for the cooling team of the Mu engine, APL's first liquid propellant engine.

An integrated engine control unit designed to fire and control liquid bi-propellant rocket engines.

Development of the Triton liquid bi-propellant engine for the Experimental Rocket Propulsion Lab

Repository for the controls and testing team of the Mu engine, APL's first liquid propellant engine.

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

Python library for internal contour development and performance calculations of liquid propellant rocket engines - Under Development

This repository has been created to publicly share the different scripts used at Carleton Propulsion Club to build the first bi-propellant liquid rocket engine!

This repository contains the raw code used to collect data from two platform load cells to measure the mass flowrate of two liquid propellants for a 1.5 kN bipropellant liquid rocket engine.