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Oblate-Earth Effects on the Calculation of Ec During Spacecraft ReentryThe bulge in the Earth at its equator has been shown to lead to a clustering of natural decays biased to occur towards the equator and away from the orbit's extreme latitudes. Such clustering must be considered when predicting the Expectation of Casualty (Ec) during a natural decay, because of the corresponding clustering of the human population in the lower latitudes. This study expands upon prior work, and formalizes in a single empirical equation the correction that must be made to the calculation of the average exposed population density as a result of this effect. The equation is represented as a function of ballistic number and inclination of the entering spacecraft over the credible range of ballistic numbers.
Document ID
20170009909
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Bacon, John B.
(NASA Johnson Space Center Houston, TX, United States)
Matney, Mark
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
October 12, 2017
Publication Date
October 18, 2017
Subject Category
Spacecraft Design, Testing And Performance
Space Transportation And Safety
Report/Patent Number
JSC-CN-39730-2
Report Number: JSC-CN-39730-2
Meeting Information
Meeting: International Association for the Advancement of Space Safety Conference (IAASS)
Location: Toulouse
Country: France
Start Date: October 18, 2017
End Date: October 20, 2017
Sponsors: International Association for the Advancement of Space Safety
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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