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Effect of probe configuration on radiative heating during Jovian entryThe radiative heating to the probe's surface and the effects of the recession of the heat shield caused by this heating are analyzed for five initial probe configurations for a Jovian entry. The initial configurations are spherically capped, conical bodies and hyperboloids. The results show that severe blunting of the nose region occurs for all configurations due to ablation of the heat shield caused by the large radiative heating rates. Recession at the nose region can possibly cause a concavity at the stagnation point. Furthermore, the recession of the heat shield, especially for the spherically capped, conical bodies, will be underpredicted if the change in the probe's shape during the entry is neglected in an analysis.
Document ID
19760054744
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sutton, K.
(NASA Langley Research Center Hampton, VA, United States)
Jones, J. J.
(NASA Langley Research Center Hampton, VA, United States)
Powell, R. W.
(NASA Langley Research Center Space Systems Div., Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 76-471
Report Number: AIAA PAPER 76-471
Meeting Information
Meeting: Thermophysics Conference
Location: San Diego, CA
Start Date: July 14, 1976
End Date: July 16, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A37710
Distribution Limits
Public
Copyright
Other

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