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Performance of entry heat shields on Pioneer Venus probesThe Pioneer Venus probes approached Venus with high relative velocity. As they entered the atmosphere, they were rapidly decelerated by aerodynamic drag, and a great deal of heat was generated. To protect the probe structure and the scientific instruments, a carbon phenolic heat shield was placed on the front of the probes. Because the design of heat shields for planetary entry is a developing technology, thermocouples were placed in the heat shields so that actual and predicted heat shield performance could be compared. The function of the heat shield is discussed, the probe environments during entry into the Venusian atmosphere are described, and some results from the heat shield experiment are presented. It was found that for the most part, the heat shields performed better than expected.
Document ID
19810042430
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Pitts, W. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Wakefield, R. M.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 11, 2013
Publication Date
December 30, 1980
Publication Information
Publication: Journal of Geophysical Research
Volume: 85
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
81A26834
Distribution Limits
Public
Copyright
Other

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