This is lecture to be given at the IPPW 2016, as part of the 2 day course on Short Course on Destination Venus: Science, Technology and Mission Architectures. The attached presentation material is intended to be introduction to entry aspects of Venus in-situ robotic missions. The presentation introduces the audience to the aerodynamic and aerothermodynamic aspects as well as the loads, both aero and thermal, generated during entry. The course touches upon the system design aspects such as TPS design and both high and low ballistic coefficient entry system concepts that allow the science payload to be protected from the extreme entry environment and yet meet the mission objectives.
Entry at Venus
International Planetary Probe Workshop ; 2016 ; Laurel, MD, United States
2016-06-13
Miscellaneous
No indication
English
NTRS | 1976
|NTRS | 2005
|Simulation of Venus atmospheric entry by earth re-entry.
AIAA | 1969
|Simulation of Venus atmospheric entry by earth re-entry
AIAA | 1968
|Challenges of a Venus entry mission
IEEE | 2011
|