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Tag Archives: Launcher

Base flow dependence on nozzle cluster configuration during ascent for a VTVL launcher

1.Events, 1.HiSST 2025, High-Speed Aerodynamics and Aerothermodynamics with application to hypersonic regimesBy Beata Wierzbińska-PrusOctober 26, 2025Leave a comment

Tamas BYKERK

DOI Number: N/A

Conference number: HiSST-2025-010

Detached eddy simulation of Callisto vehicle during subsonic retro-propulsion descent

1.Events, 1.HiSST 2025, High-Speed Missions and VehiclesBy Beata Wierzbińska-PrusOctober 21, 2025Leave a comment

Tobias ECKER

DOI Number: N/A

Conference number: HiSST-2025-341

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, 2024

Sebastian KARL, Tamas BYKERK, Mariasole LAURETI

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-034

Conference Number: HiSST-2024-034

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