ISO 27852:2016
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.
OEN:
ISO
Langue:
English
Code(s) de l'ICS:
49.140
Statut:
Annulée
Date de Publication:
2016-07-03
Numéro Standard:
ISO 27852:2016