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Effects of atmospheric structure on radiative heating for Jupiter entry probeNew estimates of the radiative heat load to a Jupiter entry probe have been obtained for revised models of Jupiter's atmosphere based on the latest data from Pioneer 10 and 11 missions and earth-based experiments. The new estimates of the radiative heat load are compared with results obtained for the previous atmospheric models. The changes in Jupiter's atmospheric models cause a substantial reduction in the radiative heat load for the atmosphere denoted as 'cool', but only moderate reductions for the atmospheres denoted as 'nominal' and 'warm'. Results are also presented showing the effects of inertial entry angle for off-equatorial entries in the revised model atmospheres.
Document ID
19780036820
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 9, 2013
Publication Date
January 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 78-185
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Huntsville, AL
Start Date: January 16, 1978
End Date: January 18, 1978
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
78A20729
Distribution Limits
Public
Copyright
Other

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