Resumen
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.
Informaciones generales
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Estado: PublicadoFecha de publicación: 2024-02Etapa: Norma Internacional publicada [60.60]
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Edición: 3Número de páginas: 48
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Comité Técnico :ISO/TC 20/SC 14ICS :49.140
- RSS actualizaciones
Ciclo de vida
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Anteriormente
RetiradaISO 27852:2016
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Ahora
