T-MATS Aircraft Design & Engineering

An open source thermodynamic modeling package completed on behalf of NASA. The Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) package offers a MATLAB/Simulink toolbox that gives a developer the ability to create simulations of such thermodynamic systems as turbomachinery and gas turbines. Keywords: TMATS, Control System, Numerical Methods, Newton-Raphson, Jacobian Calculation, Propulsion, Aircraft Engine, Jet, Turbofan, Turbojet, Compressor, Turbine, Nozzle, Inlet, open source

What T-MATS does

An open source thermodynamic modeling package completed on behalf of NASA. The Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) package offers a MATLAB/Simulink toolbox that gives a developer the ability to create simulations of such thermodynamic systems as turbomachinery and gas turbines. Keywords: TMATS, Control System, Numerical Methods, Newton-Raphson, Jacobian Calculation, Propulsion, Aircraft Engine, Jet, Turbofan, Turbojet, Compressor, Turbine, Nozzle, Inlet, open source It is a free, open-source project hosted at nasa/T-MATS and released under the Apache-2.0 licence.

Download and install

1. Get the files. Use Download releases above if the maintainers publish binaries, otherwise grab the source ZIP or git clone https://github.com/nasa/T-MATS.git.
2. Read the README. Build and runtime requirements differ per platform — the repo README is the authoritative guide.
3. Check the licence. Apache-2.0 terms apply to redistribution and commercial use.
4. Join the community. Issues, discussions and pull requests live in the repository — that is where bugs get fixed.

Project snapshot

• Repositorynasa/T-MATS
• Stars335
• Forks144
• LanguageHTML
• LicenceApache-2.0
• Last update2025-01-15

Not affiliated with the project authors. Metadata pulled from the GitHub API; figures may lag the live repository.