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.
Status: Under development
Edition: 3Number of pages: 39
Technical Committee: ISO/TC 20/SC 14 Space systems and operations
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|std 1 61|
|std 2 61||Paper|