rocket-propulsion

# Rocket Propulsion Analysis Skill ## Purpose Enable comprehensive rocket engine design and performance analysis including combustion analysis, nozzle design, and propellant optimization. ## Capabilities - CEA combustion analysis integration - Nozzle design and optimization (bell, aerospike) - Propellant selection and performance comparison - Chamber pressure and mixture ratio optimization - Regenerative cooling analysis - Injector design considerations - Thrust vectoring system analysis - Rocket Propulsion Analysis (RPA) integration ## Usage Guidelines - Use CEA for accurate combustion product calculations - Optimize mixture ratio for specific impulse or thrust requirements - Consider thermal management in chamber and nozzle design - Account for real gas effects at high pressures - Validate designs against empirical correlations and test data - Document propellant properties and compatibility considerations ## Dependencies - CEA (Chemical Equilibrium with Applications) - RPA (Rocket Propulsion Analysis) - MATLAB ## Process Integration - AE-005: Rocket Propulsion Design