thermal
CommunityEnd-to-end spacecraft thermal design.
System Documentation
What problem does it solve?
Expert spacecraft thermal control systems engineering — energy balance analysis, radiator sizing, heater power budgets, TPS material selection, cryogenic chain design, and orbit-average thermal predictions. Use when performing thermal balance calculations, sizing radiators or heat pipes, selecting thermal coatings, designing heat rejection systems, evaluating re-entry TPS, managing cryogenic boiloff, or reviewing hot/cold case bounding. Trigger with "thermal control", "radiator sizing", "heat balance", "TPS", "re-entry heating", "thermal coatings", "MLI", "heat pipe", "cryogenic", "Stefan-Boltzmann", "eclipse thermal".
Core Features & Use Cases
- End-to-end thermal design guidance for spacecraft from first principles to subsystem integration.
- Radiator sizing, heater budgeting, coatings selection, MLI and cryogenic chain considerations.
- Realistic, mission-appropriate bounding for hot and cold cases across LEO, GEO and deep space.
Quick Start
Design a radiator for a 500 W payload in LEO and verify hot/cold-case performance.
Dependency Matrix
Required Modules
None requiredComponents
Standard package💻 Claude Code Installation
Recommended: Let Claude install automatically. Simply copy and paste the text below to Claude Code.
Please help me install this Skill: Name: thermal Download link: https://github.com/devideamax/aerospace-team/archive/main.zip#thermal Please download this .zip file, extract it, and install it in the .claude/skills/ directory.
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