Evaluation of hypervelocity impact of micrometeoroids and orbital debris on next-generation space solar cells

被引:0
作者
Toyota, Hiroyuki [1 ]
Nakamura, Tetsuya [2 ]
Kanaya, Shusaku [2 ]
Sumita, Taishi [2 ]
Hirai, Takayuki [3 ]
Kobayashi, Masanori [3 ]
机构
[1] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2525210, Japan
[2] Japan Aerosp Explorat Agcy, Res & Dev Directorate, Tsukuba, Ibaraki 3058505, Japan
[3] Chiba Inst Technol, Planetary Explorat Res Ctr, Narashino, Chiba 2750016, Japan
关键词
solar cell; micrometeoroid; orbital debris; hypervelocity impact; IMM3J; perovskite; space; ARRAY;
D O I
10.35848/1347-4065/acd18b
中图分类号
O59 [应用物理学];
学科分类号
摘要
This paper discusses the hypervelocity impacts of micrometeoroids and orbital debris (MMODs) on inverted metamorphic triple-junction (IMM3J) and perovskite solar cells, which are much thinner than conventional triple-junction (3J) solar cells. We experimentally found that IMM3J solar cells can suffer from short-circuit faults due to the hypervelocity impacts of MMODs, unlike conventional 3J cells, and determined the projectile diameters and velocities that could cause them using a model proposed by Burt. No short-circuit mode was identified in perovskite solar cells, but they had open-circuit faults several days after the hypervelocity impact experiment, which are possibly attributed to the decomposition of the perovskite crystal by moisture in the air due to the broken seal.
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页数:13
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