Superseded
Standard
Historical
ISO 27852:2016
Space systems — Estimation of orbit lifetime
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Summary
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.
Notes
95.99 : Annulation de la Norme internationale
Technical characteristics
| Publisher | International Organization for Standardization (ISO) |
| Publication Date | 07/04/2016 |
| Edition | 2 |
| Page Count | 43 |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
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23/02/2024
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