Thermionic systems for DOD missions
Thermionic systems for DOD missions
复制标题
用于国防部任务的热电子系统
DOI：
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发表时间：
1991
期刊：
影响因子：
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通讯作者：
R. Dahlberg
中科院分区：
文献类型：
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作者：
J. Mills;R. Dahlberg
本文总结了1990-1991财年空军武器实验室（AFWL）电子学系统设计计划中，罗克韦尔和通用原子公司（GA）联合提出并研究的电子学系统的评估结果。评估了六个独特的不同的超导概念，包括基于超导燃料元件（FTE）的概念，泵送回路设计，热管冷却设计，快速和缓和的频谱方法，以及俄罗斯黄玉概念的衍生物。这些概念相对于其满足10至100 kWe范围内特定AFWL要求的能力进行了比较。评估导致罗克韦尔/GA选择了三个最能满足空军要求的概念：星星-C，快速驱动泵回路TFE设计，快速驱动泵回路TFE设计和快速驱动热管冷却TEF反应堆。
This paper summarizes the evaluations of candidate thermionic systems that led to the designs being jointly proposed and studied by Rockwell and General Atomics (GA) in the FY 1990–1991 Air Force Weapons Laboratory (AFWL) thermionics system design program. Six uniquely different thermionic concepts were evaluated that encompassed thermionic fuel element (FTE)‐based concepts, pumped loop designs, heat‐pipe cooled designs, fast and moderated spectrum approaches, and a derivative of the Russian TOPAZ concept. The concepts were compared relative to their ability to satisfy specific AFWL requirements over the 10‐ to 100‐kWe range. The evaluation led to the Rockwell/GA selection of three concepts that could best meet the Air Force requirements: STAR‐C, a fast driver pumped loop TFE design, and a fast driver pumped loop TFE design, and a fast driver heat–pipe cooled TEF reactor.