作者: Antonio Viviani , Giuseppe Pezzella
DOI: 10.1080/19942060.2009.11015290
关键词: Engineering 、 Crew 、 Aerospace engineering 、 Low earth orbit 、 Atmospheric entry 、 Aeronautics 、 Reentry
摘要: This paper deals with the aerothermodynamic analysis of a capsule Crew Return Vehicle concept for low Earth orbit support service. The reentry scenario corresponding loading environmen...