Abstract
ISO 27852:2016 describes a process for the estimation of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits.
It also clarifies the following:
a) modelling approaches and resources for solar and geomagnetic activity modelling;
b) resources for atmosphere model selection;
c) approaches for spacecraft ballistic coefficient estimation.
General information
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Status: WithdrawnPublication date: 2016-07Stage: Withdrawal of International Standard [95.99]
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Edition: 2Number of pages: 43
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Technical Committee :ISO/TC 20/SC 14ICS :49.140
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Life cycle
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Previously
WithdrawnISO 27852:2011
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Now
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Revised by
PublishedISO 27852:2024
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