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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.
| Author | ISO/TC 20/SC 14 Space systems and operations |
|---|---|
| Editor | ISO |
| Document type | Standard |
| Format | Paper |
| Edition | 2 |
| ICS | 49.140 : Space systems and operations
|
| Number of pages | 43 |
| Replace | ISO 27852:2011 |
| Weight(kg.) | 0.1731 |
| Year | 2016 |
| Country | Switzerland |