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