ISO 27852:2016

Status : Published (To be revised)

This standard will be replaced by ISO/FDIS 27852

	Format	Language
std 1 166	PDF + ePub
std 2 166	Paper

CHF166

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Abstract

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.

General information

Status
: Published

Publication date
: 2016-07

Stage
: International Standard to be revised [90.92]
Edition
: 2

Number of pages
: 43
Technical Committee :
ISO/TC 20/SC 14

ICS :
49.140
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