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首页> 外文期刊>Nuclear Technology >Empirical Analysis of the Multi-Mission Radioisotope Thermoelectric Generator Qualification Unit Operated at a Low Thermal Inventory with Potential for Improved End-of-Life Power
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Empirical Analysis of the Multi-Mission Radioisotope Thermoelectric Generator Qualification Unit Operated at a Low Thermal Inventory with Potential for Improved End-of-Life Power

机译:多功率放射性同位素热电发电机验证单元的实证分析在低热库存中操作,具有改进的寿命终端电力

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Performance predictions for the first multi-mission radioisotope thermoelectric generator (MMRTG) flight unit and engineering unit were recently reported. Both units were produced and operated/tested within specifications [i. e., nominal thermal inventory = 2000 W(thermal)]. In an attempt to study the effect of a deep space cruise on an MMRTG that has been operational for 6.25 years (2.25 years storage + 4 years cruise), the qualification unit (QU) was placed on life test with a below-specification thermal inventory of 1904 W(thermal). Analysis indicates that loading an MMRTG with a lower thermal inventory may result in less power at the beginning-of-life but more power at the end-of-design-life (EODL). The lower thermal inventory in the QU produces a lower operating temperature, which appears to cause a significant reduction in the degradation rate of the thermoelectric couples. Preliminary calculations indicate that a thermal inventory of 1904 W(thermal) could result in a 9 W(electric) power boost at EODL [i.e., 84 W(electric)], which is a 12% improvement over the first MMRTG flight unit and engineering unit predictions. Preliminary degradation analysis suggests that a 1904 W(thermal) unit will begin to produce more power than a 2027 W(thermal) unit approximately 4 years after fueling. This suggests that missions with a primary power requirement more than 4 years after fueling would benefit from a lower thermal inventory. In addition, using a lower thermal inventory has significant benefits for ~(238)Pu stockpile management and may allow for additional MMRTGs to be fueled from our current reserves. Conclusions and hypotheses presented here should be considered preliminary because the QU data set is very small and there are some uncertainties regarding how early-life QU data will translate into later-life performance. More QU testing at a thermal inventory of 1904 W(thermal) is needed to prove that the preliminary conclusions presented here are valid.
机译:最近报道了第一多次任务放射性电视热电发电机(MMRTG)飞行单元和工程单元的性能预测。在规范中生产和操作两个单元[i。即,标称热库存= 2000 W(热)]。为了试图研究一项在6.25年(2.25年储存+ 4年巡航)运营的MMRTG上的深度空间巡航的影响,资格单位(QU)置于使用以下规范的热量库存的生命测试1904 w(热)。分析表明,使用较低的热量库存加载MMRTG可能导致寿命开始的功率较低,但在设计端寿命(EODL)处的电力更多。曲中的较低的热量库存产生较低的工作温度,这似乎导致热电耦合的降解速率显着降低。初步计算表明,1904W(热)的热量库存可能导致eodl [IE,84 W(电)]的9 W(电动)功率升压,这是对第一MMRTG飞行单元和工程的12%改善单位预测。初步降解分析表明,1904W(热)单元将开始在加油后4年后的2027 W(热)单元产生更多的功率。这表明在加油后4年来的主要电力要求的任务将受益于较低的热量库存。此外,使用较低的热量库存对〜(238)PU库存管理具有显着的益处,并且可能允许额外的MMRTG从我们当前的储备中加油。这里呈现的结论和假设应该被认为是初步的,因为Qu数据集非常小,有关早期Qu数据如何转化为越来越寿命的性能存在一些不确定性。需要在1904W(热量)的热量库存中进行更多曲衡来证明这里呈现的初步结论有效。

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