ISO 27852:2016
Withdrawn
View Superseded by
Space systems — Estimation of orbit lifetime
Hardcopy , PDF
English
04-07-2016
09-04-2025
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.
| Committee |
ISO/TC 20/SC 14
|
| DevelopmentNote |
Supersedes ISO/DIS 27852. (07/2016)
|
| DocumentType |
Standard
|
| Pages |
43
|
| PublisherName |
International Organization for Standardization
|
| Status |
Withdrawn
|
| SupersededBy | |
| Supersedes | |
| UnderRevision |
| Standards | Relationship |
| BS ISO 27852:2016 | Identical |
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