In the frame of preliminary technological investigations for future European Mars landing probes, a study has been performed by Dassault under the supervision of ESTEC on potential thermal protection systems and aeroshell configurations for such penetrators.After an extensive trade-off between numerous candidate architectures and technologies, two solutions were more deeply investigated for feasibility assessment purposes:
Aeroshell Compared Design and Analysis for Mars Penetrators
Sae Technical Papers
International Conference On Environmental Systems ; 1994
01.06.1994
Aufsatz (Konferenz)
Englisch
Aeroshell Compared Design and Analysis for Mars Penetrators
British Library Conference Proceedings | 1994
|Online Contents | 1998
Design of a Mars entry 'Aeroshell'
Tema Archiv | 1974
|Aerothermal Study of Mars Pathfinder Aeroshell
Online Contents | 1996
|Aerothermal Study of Mars Pathfinder Aeroshell
AIAA | 1996
|