Skip to main content
Back

ISO 27852:2016

Space systems -- Estimation of orbit lifetime

General information

Withdrawn from 23.02.2024
Directives or regulations
None

Standard history

Status
Date
Type
Name
23.02.2024
Main
04.07.2016
Main
Main
ISO 27852:2011
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.

Required fields are indicated with *

*
*
*
PDF
89.37 € incl tax
Paper
89.37 € incl tax
Standard monitoring