Resumen
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.
Informaciones generales
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Estado: RetiradaFecha de publicación: 2016-07Etapa: Retirada de la Norma Internacional [95.99]
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Edición: 2Número de páginas: 43
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Comité Técnico :ISO/TC 20/SC 14ICS :49.140
- RSS actualizaciones
Ciclo de vida
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Anteriormente
RetiradaISO 27852:2011
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Ahora
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Revisada por
PublicadoISO 27852:2024
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