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Revolutionizing Spacecraft Thermal Control with Dynamic Graphene Radiators: SmartSat

Revolutionizing Spacecraft Thermal Control with Dynamic Graphene Radiators: SmartSat
利用动态石墨烯散热器彻底改变航天器热控制:SmartSat
批准号:
10098641
负责人:
金额:
$269.79万
依托单位:
依托单位国家:
英国
项目类别:
EU-Funded
财政年份:
2024
资助国家:
英国
项目状态:
未结题
起止时间:
2024 至 --

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中文摘要
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英文摘要
Satellites face numerous technological challenges due to the extreme temperature variations they experience while orbiting the Earth. These temperature fluctuations pose a significant risk to the delicate electronic and optical systems within the satellite, as overheating or overcooling can cause catastrophic damage. To maintain thermal stability, a satellite's heat controller must balance venting the internal heat generated by onboard systems with insulating the craft from solar radiation and continuously radiating the heat. This task is particularly challenging since thermal radiation is the only means to dissipate excess heat from the satellite. The sun-facing side of a satellite can be up to +200°C hotter than the side exposed to the cold vacuum of space, resulting in a rapid temperature change of >200°C when the satellite enters Earth's shadow. Traditional temperature control systems, such as passive radiators, are designed to reflect solar radiation and emit infrared light through thermal radiation. However, these radiators cannot be switched off or adjusted according to the satellite's position relative to the Earth and the Sun. This limitation can lead to rapid cooling of internal systems and components when the satellite enters Earth's shadow, causing temperature-induced stress and damage to delicate electronics. Engineers utilize large but delicate solar shields, bulky thermal louvres, heat pipes, and heaters to manage these temperature extremes. However, these thermal control systems are not only heavy but also consume a significant amount of available power. This increased weight and power consumption reduce the payload capacity and overall efficiency of the satellite. An ideal thermal control system would adapt to changing thermal conditions in real-time, maintaining optimal temperatures for the satellite's electronic systems and components. By modulating its heat dissipation capabilities based on the satellite's position, an innovative adaptive thermal management system would not only improve satellite performance and reliability but also significantly extend operational lifespan, making satellites more cost-effective and efficient for manufacturers and operators. As the space market experiences a critical shift with decreasing launch costs and increasing launch frequency, satellite manufacturers and operators are under pressure to optimize efficiency and maintain profitability. Consequently, there is an urgent need for a lightweight, low-cost, and low-power consumption solution to enhance satellite efficiency (e.g., by increasing data throughput while reducing payload and power consumption) and enable the long-lasting use of small satellites. Such an innovative solution would make previously unattainable projects feasible and usher in a new era of satellite technology.
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