首页> 外文期刊>Progress in Nuclear Energy >AN ANALYSIS OF COATED PARTICLES FUEL COMPACT-GENERAL PURPOSE HEAT SOURCE (CPFC-GPHS)
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AN ANALYSIS OF COATED PARTICLES FUEL COMPACT-GENERAL PURPOSE HEAT SOURCE (CPFC-GPHS)

机译:包覆颗粒燃料通用目的热源(CPFC-GPHS)的分析

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摘要

The Coated Particles Fuel Compact (CPFC) offers performance advantages for use in the Radioisotope Heater Unit (RHU) and General Purpose Heat Source (GPHS) for Advanced Radioisotope Power Systems (ARPSs), generating a few milliwatts or a few hundred watts of electrical power, respectively, for future planetary exploration. It comprises ~(238)PuO_2 fuel kernels with 5-μm thick PyC inner coating and a strong ZrC outer coating, dispersed in a graphite matrix. The fuel kernels in the compact could be either of a single size (≤ 1200 μm) or binary sizes (300 and 1200 μm) for particles' volume compaction of 62.5% and 72%, respectively. The ZrC coating serves as a pressure vessel for containing the fuel kernels and the helium gas generated by the radioactive decay of ~(238)Pu during storage time before launch and the mission lifetime (15-25 years). The thickness of the ZrC coating and hence, the specific thermal power of the CPFC depend on the estimated maximum fuel temperature during reentry following a launch accident, the storage time before launch and mission duration, and the helium release fraction from the fuel kernels. This paper investigates the advantage of replacing the four iridium-clad ~(238)PuO_2 fuel pellets, the two floating graphite membranes, and the two graphite impact shells in current State-Of-the-Art (SOA) GPHS with CPFC. The mass, thermal power, and specific thermal power of the CPFC-GPHS are calculated as functions of the helium release fraction from the fuel kernels, up to a full release, and the maximum compact temperature during reentry, from 1500 K to 2400 K. For the same mass and volume, the single-size particles CPFC-GPHS could generate 260 W at Beginning-Of-Mission (BOM), following 10 years of storage, versus 231 W for SOA GPHS. For an additional 10% higher mass, the CPFC-GPHS could generate 340 W at BOM at a specific thermal power of 214 W/kg, which are 47% and 34% higher than those of SOA GPHS, respectively.
机译:包覆颗粒燃料复合材料(CPFC)具有性能优势,可用于高级放射性同位素动力系统(ARPS)的放射性同位素加热器单元(RHU)和通用热源(GPHS),产生几毫瓦或几百瓦的电能分别用于未来的行星探索。它包含〜(238)PuO_2燃料核,具有5μm厚的PyC内涂层和强ZrC外部涂层,分散在石墨基质中。压块中的燃料仁可以是单一尺寸(≤1200μm),也可以是二元尺寸(300和1200μm),分别使颗粒的体积压缩率为62.5%和72%。 ZrC涂层用作压力容器,用于容纳燃料核和由发射前的存储时间内〜(238)Pu的放射性衰变产生的氦气和任务寿命(15-25年)。 ZrC涂层的厚度,以及由此而来的CPFC的比热功率,取决于发射事故后重返过程中估计的最高燃料温度,发射前的存储时间和任务持续时间,以及燃料核中的氦释放分数。本文研究了用CPFC代替当前最新(SOA)GPHS中的四个铱包覆〜(238)PuO_2燃料芯块,两个浮置石墨膜和两个石墨冲击壳的优势。 CPFC-GPHS的质量,热功率和比热功率是根据燃料内核中的氦释放分数(直至完全释放)和再入过程中的最高紧凑温度(从1500 K到2400 K)计算的。对于相同的质量和体积,存储10年后,单一尺寸的粒子CPFC-GPHS在发射开始(BOM)时可以产生260 W,而SOA GPHS则为231W。如果再增加10%的质量,CPFC-GPHS可以以214 W / kg的比热功率在BOM上产生340 W,分别比SOA GPHS高47%和34%。

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