Perform spacecraft thermal energy balance, radiator sizing, and heater budgeting calculations.
npx skills add https://github.com/devideamax/aerospace-team --skill thermal
Please help me install this Agent Skill. Skill: thermal Source: https://github.com/devideamax/aerospace-team/tree/main/skills/thermal Command: npx skills add https://github.com/devideamax/aerospace-team --skill thermal
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".
Design a radiator for a 500 W payload in LEO and verify hot/cold-case performance.
High-intent search queries and answers about installing and using this skill.
Spacecraft radiator sizing is calculated by performing an energy balance to determine heat rejection load, then applying two-sided radiator equations to size required area for hot and cold case bounding.
Heater power budgeting for eclipse thermal conditions is estimated by calculating orbit-average thermal predictions and bounding the cold case to determine minimum heater wattage needed to maintain temperature limits.
Energy balance analysis for cryogenic chain design works by applying Stefan-Boltzmann equations and MLI properties to quantify heat leak, enabling prediction of cryogenic boiloff rates across LEO, GEO, and deep space orbits.
Yes, this thermal control workflow evaluates re-entry heating and TPS material selection by applying energy-balance equations to evaluate thermal protection system performance under high heat flux conditions.
Yes, this spacecraft thermal design approach supports thermal coatings selection and MLI integration by comparing surface optical properties to achieve realistic mission-appropriate energy balance across LEO, GEO, and deep-space environments.
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