ISO 27852:2016
$46.15
Space systems — Estimation of orbit lifetime
| Published By | Publication Date | Number of Pages |
| ISO | 2016-07 | 50 |
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.
