Publication date: 11th March 2026
Emerging photovoltaics (PV), including organic PV (OPV), perovskite PV (PPV), and quantum dots PV (QDPV), have attracted significant interest for aerospace applications due to their high specific power (power-to-weight ratio), high mechanical flexibility, and low cost. For example, OPV, PPV, and QDPV exhibit specific powers of 39.3, 50, and 15.2 W/g, respectively, which are significantly higher than those of traditional PV. [1-3] High-altitude pseudo-satellites (HAPS) operating in the lower stratosphere (∼20–25 km) could be the first to deploy these emerging PV technologies. This region exposes photovoltaic systems to AM0 solar irradiance, and the environmental conditions include low-temperature cycles (+10 → –20 °C during the day and to –85 °C at night), and low ambient pressures that differ significantly from terrestrial conditions.[4] These environmental stresses can critically impact emerging PV, yet direct comparative studies across material classes are scarce. In this work, we investigate the low-temperature performance and thermal cycling stability of these three promising PV technologies under conditions mimicking HAPS environments.
For OPV, two state-of-the-art active-layer material systems have been studied and revealing acceptor-dependent performance differences at reduced temperatures. In contrast, for QDPV, different hole-transport layer configurations were studied here, showing that PbS-MPA devices maintained or slightly improved power conversion efficiency (PCE) even in an HAPS environment and down to −100 °C, and exhibited excellent thermal cycling stability, suggesting robustness under repeated stratospheric day–night cycles. Furthermore, Perovskite devices with both narrow, wide-bandgap compositions and tandem were evaluated on rigid and flexible substrates, demonstrating high PCEs under HAPS environment for tandem PV.
Interesting: the QDPV retains 100% of its initial PCE even at -100 °C, whereas the PPV and OPV retain ~80% and ~50% of their initial PCE, respectively, under similar conditions. Furthermore, the QDPV and PPV showed excellent thermal cycling stability over the range of +20 to -85 °C, with 15 cycles.
Our comparative study highlights material-dependent responses to stratospheric stresses, identifies design pathways for improved environmental resilience, and provides important initial data for the selection for next-generation lightweight power systems deployed in HAPS and related aerospace applications.
R.D. and W.C.T gratefully acknowledges financial support from the SPECIFIC Innovation and Knowledge Centre (EP/N020863/1) and the ATIP programme (EP/T028513/1). Hin-Lap Yip acknowledges funding from the Guangdong Major Project of Basic and Applied Basic Research (No. 2019B030302007) and the Ministry of Science and Technology of China (No. 2019YFA0705900). Guichuan Zhang acknowledges financial support from the National Natural Science Foundation of China (No. 51903095) and the Natural Science Foundation of Guangdong Province (No. 2021A1515010959). Z.L. acknowledges support from the National Natural Science Foundation of China (Grant No. 52372215). L.L. and H.T. acknowledge financial support from the National Natural Science Foundation of China (U21A2076, 62305150, 52427803, and 62474086) and the Natural Science Foundation of Jiangsu Province (BK20232022, BE2022021, and BE2022026). The authors gratefully acknowledge these funding bodies for their support of the research activities reported in this work.
