Aerodynamic Data Set Generation for the Experimental Vehicle ReFEx
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Publisher
Springer International Publishing
Link
https://link.springer.com/content/pdf/10.1007/978-3-030-79561-0_13
Reference5 articles.
1. Rickmers, P., et al.: Refex: reusability flight experiment a flight experiment to demonstrate controlled aerodynamic flight from hypersonic to subsonic velocities with a winged rlv. In: 7th European Conference for Aeronautics and Space Sciences (EUCASS). https://doi.org/10.13009/EUCASS2017-644 (2017)
2. Merrem, C., Wartemann, V., Eggers, T.: Preliminary aerodynamic design of a reusable booster flight experiment. CEAS Space J. 12(3), 429–439 (2020). https://doi.org/10.1007/s12567-020-00313-9
3. NN Aerodynamic Design Data Book – Orbiter Vehicle STS-1. Rockwell International, USA (1980)
4. Merrem, C., Kiehn, D., Wartemann, V., Eggers, T.: Aerodynamic design of a reusable booster stage flight experiment. In: 8th European Conference for Aeronautics and Space Sciences (EUCASS). https://doi.org/10.13009/EUCASS2019-644 (July 2019)
5. Weiland, C.: Aerodynamic Data of Space Vehicles. Springer Science & Business Media (2014)
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1. Design of ReFEx Guidance: Periodic On-Board Trajectory Updates;AIAA SCITECH 2024 Forum;2024-01-04
2. Design of ReFEx Guidance: Trajectory Correction after Ascent;AIAA SCITECH 2023 Forum;2023-01-19
3. Design of a Control Allocation Solution for the Winged Reusable Launch Vehicle ReFEx;AIAA SCITECH 2022 Forum;2022-01-03
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