a5c-ai Spacecraft Thermal Analysis Skill
Purpose
Provide comprehensive spacecraft thermal control system design and analysis capabilities for component temperature prediction and thermal management.
Capabilities
- Thermal Desktop and SINDA modeling
- Orbital environment definition
- Radiator sizing and placement
- Heater control logic design
- Thermal balance verification
- Hot/cold case analysis
- Component temperature prediction
- MLI and coating specification
Usage Guidelines
- Define worst-case thermal environments for hot and cold cases
- Use appropriate view factors and orbital parameters
- Size radiators with adequate margin for degradation
- Design heater circuits with redundancy for critical components
- Validate thermal models against test data
- Document thermal control system design and operating procedures
Dependencies
- Thermal Desktop
- SINDA/FLUINT
- ESATAN
Process Integration
- AE-015: Spacecraft Thermal Analysis