Tag Archives: Reusable Flight Experiment ReFEx

Aerothermal Loads Analysis of ReFEx by coupled CFD Calculations

1.Events, High-Speed Missions and Vehicles, HiSST 2024By Beata Wierzbińska-Prus May 16, 2024

Marius FRANZE, Viola WARTEMANN, C. MERREM, Henning ELSÄSSER, Tobias RUHE, Thino EGGERS, Hendrik WEIHS

DOI Number: N/A

Conference number: HiSST-2024-113

Rolling Capabilities of the experimental Vehicle ReFEx

1.Events, High-Speed Missions and Vehicles, HiSST 2022By tvermin April 12, 2024

C. Merrem, V. Wartemann, H. Elsässer, T. Ruhe, Th. Eggers

DOI Number XXX-YYY-ZZZ

Conference Number HiSST-2022-36

Preliminary Aerodynamic Design of a Reusable Booster Flight Experiment

High-Speed Missions and Vehicles, HiSST 2018, Hypersonic Aerodynamics, Space Launch Vehicles, Supersonic and Hypersonic Aircraft DesignBy tvermin October 13, 2023

Merrem , V. Wartemann , Th. Eggers

DOI Number XXX-YYY-ZZZ
Conference Number HiSST 2018_1870857