钙钛矿(结构)
材料科学
空间环境
薄膜
光伏
退火(玻璃)
光电子学
光伏系统
卤化物
航空航天
航空航天材料
纳米技术
航空航天工程
化学工程
电气工程
化学
复合材料
物理
工程类
无机化学
地球物理学
作者
Lyndsey McMillon‐Brown,William Delmas,Samuel Erickson,Jorge Arteaga,Mark Woodall,Michael Scheibner,Timothy A. Krause,Kyle Crowley,Kaitlyn T. VanSant,Joseph M. Luther,Jennifer N. Williams,Jeremiah McNatt,Sayantani Ghosh
标识
DOI:10.1109/pvsc48320.2023.10359710
摘要
In support of NASA's Artemis program with the goal of a sustained human-lunar presence, there is a need for very large (>100kW) and high-voltage-capable solar arrays, estimated to cost over $150M. Perovskite-based thin-film photovoltaics offer substantial advantages over state-of-the-art solar arrays from the perspective of manufacturing large arrays. Perovskites have also demonstrated some of the lowest temperature coefficients and highest defect tolerance, which make them excellent candidates for aerospace applications. However, metal halide perovskites (MHP) must demonstrate durability in space which presents different challenges than terrestrial operating environments. To decisively test the viability of perovskites being used in space, a perovskite thin film is positioned in low earth orbit for 10 months on the International Space Station, which was the first long-duration study of an MHP in space. Postflight high-resolution ultrafast spectroscopic characterization and comparison with control samples reveal that the flight sample exhibits superior photo-stability, no irreversible radiation damage, and a suppressed structural phase transition temperature by nearly 65 K, broadening the photovoltaic operational range. Further, significant photo-annealing of surface defects is shown following prolonged light-soaking postflight. These results emphasize that methylammonium lead iodide can be packaged adequately for space missions, affirming that space stressors can be managed as theorized.
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