Results of studies performed for entries into Saturn, Uranus, and Neptune atmospheres with HEEET as the candidateTPS. Margined material thicknesses are compared to loom limits, and CFD-based environments are used in material sizing.
Exploration of Atmospheric Entries at Saturn, Uranus & Neptune with HEEET as Heatshield TPS
International Conference on Flight vehicles, Aerothemodynamics and Re-entry Missions (FAR 2019) ; 2019 ; Monopoli, Italy
2019-10-01
Sonstige
Keine Angabe
Englisch