Babysitter rocket-propulsion
Comprehensive skill for rocket engine design and performance analysis
install
source · Clone the upstream repo
git clone https://github.com/a5c-ai/babysitter
Claude Code · Install into ~/.claude/skills/
T=$(mktemp -d) && git clone --depth=1 https://github.com/a5c-ai/babysitter "$T" && mkdir -p ~/.claude/skills && cp -r "$T/library/specializations/domains/science/aerospace-engineering/skills/rocket-propulsion" ~/.claude/skills/a5c-ai-babysitter-rocket-propulsion && rm -rf "$T"
manifest:
library/specializations/domains/science/aerospace-engineering/skills/rocket-propulsion/SKILL.mdsource content
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