The climate impact of hydrogen-powered hypersonic transport

HIGHLIGHTS

SUMMARY

    The two hypersonic aircraft designs considered here are the models ZEHST (Zero Emission High-Speed Transport) and LAPCAT PREPHA (Programme de REcherche et de technologie sur la Propulsion Hypersonique Avancée, Falempin et_al, 1998; Scherrer et_al, 2016), with cruise altitudes at approximately 26 and 35 km, respectively. In Dynamic Ecosystems, version 1.9) dynamical vegetation model (Krinner et_al, Atmos. Phys., 22, 14323-14354, 2022 J. Pletzer et_al. Deviations from model to observations are a cold bias, with a vertical maximum at 200 hPa and values of ±4 K (Fig 12, Jöckel et_al, 2016 . . .

     

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