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Modeling of Radiative Heating in Base Region of Jovian Entry ProbeA theoretical model is derived to determine the average thermodynamic properties in the expanding region, recirculating region, recompression region, and neck region through application of one-dimensional conservation equations. Radiative transfer is calculated using spectrally detailed computer codes accounting for nonequilibrium. The results show that the most severe heating occurs immediately behind the frustum, and that the recompression and neck regions are the major sources of radiation that heats the base stagnation point, The radiation flux to the base point is slightly stronger with ablation than without. Its value is 0.11(43 P(sub b)/P(sub s))(sup 2) times that to the front stagnation point where the base pressure P(sub b) is defined as the average pressure in the recirculating region and P(sub s) is the front stagnation-point pressure. The time-integrated heat load to the base point is 18(43 P(sub b)/P(sub s))(sup 2) kJ/sq cm.
Document ID
19980213257
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Park, Chul
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1979
Publication Information
Publication: Entry Heating and Thermal Protection
Volume: 69
Subject Category
Lunar And Planetary Exploration
Report/Patent Number
AIAA Paper 79-0039
NAS 1.15:207857
NASA/TM-1979-207857
Report Number: AIAA Paper 79-0039
Report Number: NAS 1.15:207857
Report Number: NASA/TM-1979-207857
Meeting Information
Meeting: Aerospace Sciences
Location: New Orleans, LA
Country: United States
Start Date: January 15, 1979
End Date: January 17, 1979
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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