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Phosphonic-acid-reinforced polymer hole transport layers for deployable p-i-n perovskite photovoltaics

  • Calton J. Kong
  • , Kelly R. Schutt
  • , Mohin Sharma
  • , Walker Arce
  • , Mritunjaya Parashar
  • , Ross A. Kerner
  • , Shuai You
  • , Darius Kuciauskas
  • , Robert Tirawat
  • , Ryan DeCrescent
  • , Tatchen Buh Kum
  • , Kaitlyn T. VanSant
  • , Brian M. Wieliczka
  • , Hadi Afshari
  • , Ian R. Sellers
  • , Michael D. McGehee
  • , Karen Stelling
  • , Bibhudutta Rout
  • , Kai Zhu
  • , Ahmad R. Kirmani
  • Joseph M. Luther
  • National Renewable Energy Laboratory
  • University of California at Berkeley
  • University of North Texas
  • University of Nebraska-Lincoln
  • University of Colorado Boulder
  • Rochester Institute of Technology
  • University of Oklahoma

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

The long-term durability prospects of halide perovskite solar cells are rapidly improving; however, the interface between the hole transport layer (HTL) and the perovskite remains a source of degradation. Alone, polymer- or carbazole-based HTLs suffer from incomplete coverage of the underlying indium tin oxide glass, leading to degradation and compromised performance. Here, we show a multi-HTL approach whereby a polymer HTL is reinforced using a phosphonic acid modification leading to better protection of the buried perovskite interface and more columnar growth of perovskite film, resulting in an ∼40-mV open-circuit voltage (VOC) improvement indicative of suppressed interfacial recombination across multiple p-i-n device architectures. Solar cells with this reinforced HTL show higher tolerance to several accelerated stress tests. We report, among the best durabilities for unencapsulated cells, a T90 ∼3,000 h (T80 ∼5,900 h) at 65°C under continuous 1.2 sun AM 1.5G illumination and maximum power point tracking, representing a nearly 4-fold increase compared with [2-(9H-carbazol-9-yl)ethyl]phosphonic acid (2PACz)-only devices. Furthermore, we deployed a device with this reinforced HTL on a cube satellite, with long-duration operational space testing results exceeding T80 for the complete mission duration of ∼100 days in low Earth orbit.

Original languageEnglish
Article number100431
JournalNewton
DOIs
StateAccepted/In press - 2026

Keywords

  • CubeSat
  • flight heritage
  • low Earth orbit
  • perovskite solar
  • perovskites
  • radiation tolerance
  • space photovoltaics
  • space power
  • specific power

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