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