ISO-27852 › Space systems - Estimation of orbit lifetime
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This document describes a process for the long-duration orbit lifetime prediction of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits after mission phase (including any mission lifetime extensions).
The document also clarifies:
a) modelling approaches and resources for solar and geomagnetic activity modelling;
b) resources for atmosphere model selection;
c) approaches for spacecraft ballistic coefficient estimation.
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Document Number
ISO 27852:2024
Revision Level
3RD EDITION
Status
Current
Publication Date
Feb. 1, 2024
Committee Number
ISO/TC 20/SC 14