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Some Aerothermodynamic Aspects of ESA Entry Probes 被引量:2
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作者 L.MARRAFFA F.MAZOUE +1 位作者 ph.reynier C.REIMERS 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2006年第2期126-133,共8页
Two different entry vehicles are presented here: the Inflatable Reentry and Descent Demonstrator (IRDT), and Huygens. Both missions involve (re)entries at conditions close to orbital, and have been performed in 2... Two different entry vehicles are presented here: the Inflatable Reentry and Descent Demonstrator (IRDT), and Huygens. Both missions involve (re)entries at conditions close to orbital, and have been performed in 2005. Specific aspects of the design and the mission of IRDT are briefly outlined. The preliminary results of the recent flight of IRDT and the methodology followed at ESTEC for the assessment of radiative fluxes for Huygens are summarised. 展开更多
关键词 REENTRY radiation AEROTHERMODYNAMICS heat shield CFD non-equilibrium flow entry probe
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