ISO 27852:2016
Space systems — Estimation of orbit lifetime
Reference number
ISO 27852:2016
Edición 2
2016-07
Retirada
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ISO 27852:2016
68572
Retirada (Edición 2, 2016)

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

  •  : Retirada
     : 2016-07
    : Retirada de la Norma Internacional [95.99]
  •  : 2
     : 43
  • ISO/TC 20/SC 14
    49.140 
  • RSS actualizaciones

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