有效载荷(计算)
航天器
电
核工程
电池(电)
核能
环境科学
可靠性(半导体)
航空航天工程
汽车工程
工程类
电气工程
功率(物理)
计算机科学
物理
核物理学
计算机网络
量子力学
网络数据包
作者
홍진태,손광재,김종범,박종한,안동규,양동열
标识
DOI:10.7736/kspe.2016.33.4.271
摘要
For a stable electric power supply in the space, nuclear batteries have been used as the main power source in a spacecraft owing to their long lifetime and high reliability. In accordance with the plan for lunar mission in Korea, nuclear batteries will supply electricity to the rover that needs to be developed. According to the information about the estimated payload, Korea Atomic Energy Research Institute started with the conceptual design based on the previous studies in USA and Russia. Because a nuclear battery converts the decay heat of the radioisotope into electricity, thermal design, radiation shield, and shock protection need to be considered. In this study, two types of nuclear batteries, radial type and axial type, were designed according to the alignment of the thermoelectric module. Heat transfer analyses were performed to compare their thermoelectric efficiency, and test mockups were fabricated to evaluate their performances.
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