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.
WITHDRAWN
ISO 27852:2011
95.99
Withdrawal of Standard
Jul 4, 2016
PUBLISHED
ISO 27852:2016
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