This document describes a process for the long-duration orbit lifetime prediction of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits after mission phase (including any mission lifetime extensions).
The document also clarifies:
a) modelling approaches and resources for solar and geomagnetic activity modelling;
b) resources for atmosphere model selection;
c) approaches for spacecraft ballistic coefficient estimation.
| File Size : | 1
file
, 6.8 MB |
| Note : | This product is unavailable in Ukraine, Russia, Belarus |
| Published : | 02/01/2024 |
