Abstract

SummaryMonolithic [Cs0.05(MA0.17FA0.83)0.95]Pb(I0.83Br0.17)3/Cu(In,Ga)Se2 (perovskite/CIGS) tandem solar cells promise high performance and can be processed on flexible substrates, enabling cost-efficient and ultra-lightweight space photovoltaics with power-to-weight and power-to-cost ratios surpassing those of state-of-the-art III-V semiconductor-based multijunctions. However, to become a viable space technology, the full tandem stack must withstand the harsh radiation environments in space. Here, we design tailored operando and ex situ measurements to show that perovskite/CIGS cells retain over 85% of their initial efficiency even after 68 MeV proton irradiation at a dose of 2 × 1012 p+/cm2. We use photoluminescence microscopy to show that the local quasi-Fermi-level splitting of the perovskite top cell is unaffected. We identify that the efficiency losses arise primarily from increased recombination in the CIGS bottom cell and the nickel-oxide-based recombination contact. These results are corroborated by measurements of monolithic perovskite/silicon-heterojunction cells, which severely degrade to 1% of their initial efficiency due to radiation-induced recombination centers in silicon.

Highlights

  • Multijunction solar cells that combine complementary absorber materials to selectively harvest the available solar spectrum with minimal thermalization losses power modern energy demanding satellites, spacecraft, and exploration rovers.[1]

  • We find that perovskite/silicon tandem solar cells are unsuitable for space, whereas perovskite/CIGS tandems are radiation-hard, promising cheap, flexible, and ultra-lightweight space photovoltaics

  • Our results show that perovskite/silicon heterojunction (SHJ) tandem solar cells degrade severely to 1% of their initial efficiency while perovskite/CIGS tandem solar cells retain over 85% of their initial efficiency under AM0 solar illumination even after 68 MeV proton irradiation at a dose of 2 3 1012 p+/cm[2]

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Summary

Introduction

Multijunction solar cells that combine complementary absorber materials to selectively harvest the available solar spectrum with minimal thermalization losses power modern energy demanding satellites, spacecraft, and exploration rovers.[1] While terrestrial photovoltaic (PV) systems require high-power-area (W/m2) ratios, space. PV systems require high specific power (W/g) to minimize the stowed volume, weight, inertia, and atmospheric drag of the spacecraft.[2] In addition, the cost of space PV modules ($/W) is becoming increasingly important given the growing demand for smaller, cheaper satellites[3] and the emerging privatization of space exploration,[4] both of which are revolutionizing space economics. Slow epitaxial absorber growth and high material costs render such III-V-based multijunction solar cells expensive and their mass production challenging.[7] Less expensive space-tested single-junction technologies based on crystalline silicon (c-Si),[8,9] Cu(In,Ga)Se2 (CIGS),[10]

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