Abstract
ISO 27852:2011 describes a process for the estimation of orbit lifetime for satellites, launch vehicles, upper stages and associated debris in LEO-crossing orbits.
ISO 27852:2011 also clarifies the modelling approaches and resources for solar and geomagnetic activity modelling; the resources for atmosphere model selection; and an approach for satellite ballistic coefficient estimation.
General information
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Status: WithdrawnPublication date: 2011-07Stage: Withdrawal of International Standard [95.99]
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Edition: 1Number of pages: 28
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Technical Committee :ISO/TC 20/SC 14ICS :49.140
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Life cycle
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Now
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Revised by
WithdrawnISO 27852:2016