ISO/DIS 27852

Space systems — Estimation of orbit lifetime

General information

Current stage: 40.99 Effective date: Dec 21, 2022

Originator: ISO

Owner: ISO/TC 20/SC 14

Type: International Standard

ICS: 49.140

Languages: English

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Status: Draft

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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

Revises
ISO 27852:2016

NOW

IN_DEVELOPMENT
ISO/DIS 27852
40.99 Full report circulated: DIS approved for registration as FDIS
Dec 21, 2022

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