Skill for spacecraft thermal control system design and analysis
name spacecraft-thermal description Skill for spacecraft thermal control system design and analysis allowed-tools ["Read","Write","Glob","Grep","Edit","WebFetch","WebSearch","Bash"] metadata {"version":"1.0","category":"aerospace-engineering","tags":["space-systems","thermal-control","analysis","design"]} 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