A modern tool for analyzing rocket propulsion systems using NASA-CEA data. This application provides advanced rocket nozzle design, analysis, and visualization capabilities.
- Parse and analyze NASA-CEA output files
- Interactive data visualization and filtering
- Multiple nozzle design methods:
- Method of Characteristics (MOC)
- Rao Optimum Nozzle
- Conical Nozzle
- Bell Nozzle
- Truncated Ideal Contour (TIC)
- Performance calculations and optimization
- Export capabilities (CSV, Excel, PDF)
- Graphical user interface with PyQt5
# Clone the repository
git clone https://github.com/yourusername/cea_analyzer.git
cd cea_analyzer
# Install dependencies
pip install -r requirements.txtpython -m cea_analyzerOr run directly:
python cea_analyzer/main.py- Python 3.8 or higher
- Dependencies listed in
requirements.txt