ISO 27852
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ISO 27852
85364

Status : Under development

Abstract

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.

General information

  •  : Under development
     : 2024-02
    : International Standard under publication [60.00]
  •  : 3
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

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