Containment methods for the atmospheric reentry of satellites

2020 ◽  
Vol 7 (3) ◽  
pp. 390-396
Author(s):  
Njord Eggen ◽  
Tiago Soares ◽  
Luisa Innocenti
Keyword(s):  
2011 ◽  
Vol 42 (3) ◽  
pp. 221-228 ◽  
Author(s):  
Toshio Ogasawara ◽  
Takuya Aoki ◽  
Mohamed Sayed Aly Hassan ◽  
Yosuke Mizokami ◽  
Naoyuki Watanabe

2012 ◽  
Vol 2012 ◽  
pp. 1-8 ◽  
Author(s):  
Ojas Joshi ◽  
Pénélope Leyland

During atmospheric reentry, radiative heating is one of the most important component of the total heat flux. In this paper, we investigate how the thermal radiation coming from the postshock region interacts with the spacecraft structure. A model that takes into account the radiation reflected by the surface is developed and implemented in a solid solver. A partitioned algorithm performs the coupling between the fluid and the solid thermal fields. Numerical simulation of a hollow cone head and a deployed flap region shows the effects of the radiative cooling and the significance of the surface radiation.


2016 ◽  
Vol 68 (11) ◽  
pp. 1295-1306 ◽  
Author(s):  
Minseok Jung ◽  
Hisashi Kihara ◽  
Ken-ichi Abe ◽  
Yusuke Takahashi

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