“…The nvPM acts as the primary source of condensation nuclei in the "soot-rich" regime, defined when the soot number emissions index (EIn) exceeds 10 13 kg -1 , while ambient aerosols, organic and sulfuric particles can nucleate under "soot-poor" conditions (EIn < 10 13 kg -1 ). Most kerosene-burning aircraft engines typically have nvPM EIn of 10 14 -10 16 kg -1 (EASA, 2021; Petzold et al, 1999;Moore et al, 2017;Durdina et al, 2017), and for these aircraft types, in-situ measurements and modelling studies show that the nvPM EIn influences various contrail properties and associated climate forcing (Voigt et al, 2021;Bräuer et al, 2021b;Teoh et al, 2022a;Jeßberger et al, 2013;Kärcher, 2016). However, there is a small but increasing share of aircraft types powered by staged combustors with nvPM EIn as low as ~10 11 kg -1 (EASA, 2021; Boies et al, 2015), for which the initial contrail properties need further investigation (Voigt et al, 2022).…”