Design of a Truncated Ideal Nozzle for a Re-usable First Stage Launcher 1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-PrusMay 8, 2024Sebastian KARL, Tamas BYKERK, Mariasole LAURETI DOI Number: https://doi.org/10.82241/ceas-hisst-2024-034 Conference Number: HiSST-2024-034
