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ISO 27852:2016

Space systems — Estimation of orbit lifetime

Jul 4, 2016
95.99   Withdrawal of Standard   Feb 23, 2024

General information

95.99     Feb 23, 2024

ISO

ISO/TC 20/SC 14

International Standard

49.140  

English  

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Scope

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.

Life cycle

PREVIOUSLY

WITHDRAWN
ISO 27852:2011

NOW

WITHDRAWN
ISO 27852:2016
95.99 Withdrawal of Standard
Feb 23, 2024

REVISED BY

PUBLISHED
ISO 27852:2024