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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 clustering of the human population in the same lower latitudes. This study expands upon prior work, and formalizes the correction that must be made to the calculation of the average exposed population density as a result of this effect. Although a generic equation can be derived from this work to approximate the effects of gravitational and atmospheric perturbations on a final decay, such an equation averages certain important subtleties in achieving a best fit over all conditions. The authors recommend that direct simulation be used to calculate the true Ec for any specific entry as a more accurate method. A generic equation is provided, represented as a function of ballistic number and inclination of the entering spacecraft over the credible range of ballistic numbers.
Document ID
20170009908
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Bacon, John B.
(NASA Johnson Space Center Houston, TX, United States)
Matney, Mark J.
(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
Report/Patent Number
JSC-CN39730-1
Report Number: JSC-CN39730-1
Meeting Information
Meeting: International Association for the Advancement of Space Safety (IAASS)
Location: Toulouse
Country: France
Start Date: October 18, 2017
End Date: October 20, 2017
Sponsors: International Space Safety Foundation
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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