Space‐ and Post‐Flight Characterizations of Perovskite and Organic Solar Cells

Perovskite and organic solar cells are promising for space applications for enabling higher specific powers or alternative deployment systems. However, terrestrial tests can only mimic space conditions to a certain extent. Herein, a detailed analysis of irradiation‐dependent photovoltaic parameters of perovskite and organic solar cells exposed to space conditions during a suborbital flight is presented. In orbital altitudes, perovskite and organic solar cells reach power‐conversion efficiencies of more than 13% and 6%, respectively. Based on postflight grazing‐incidence small‐angle and wide‐angle X‐ray scattering, the active layer morphology and crystalline structure of the returned space solar cells are studied and compared to those of reference solar cells that stayed in an inert atmosphere. Minor changes in the active layer morphology are induced by the sole transport, without causing significant performance loss. For the space solar cells, morphological changes are attributed to the flight experiment that includes rocket launch, spaceflight, and reentry, as well as short‐terrestrial environment exposure before and after launch. In contrast, no significant changes to the crystalline phase are observed. The notable performance during flight and high active layer stability, especially of perovskite solar cells, are promising results for further steps toward an orbital demonstration. I–V measurements of perovskite and organic solar cells during spaceflight are related to solar irradiance, yielding power‐conversion efficiencies of up to 13%. Subsequent morphology analysis with X‐Ray scattering shows minor morphological changes but promising structural stability of the solar cells that went to space.