Abstract Preview

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

  • Status :  Published
    Publication date : 2016-07
  • Edition : 2
    Number of pages : 43
  • :
    ISO/TC 20/SC 14
    Space systems and operations
  • 49.140
    Space systems and operations

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