Abstract 

ISO 27852:2011 describes a process for the estimation of orbit lifetime for satellites, launch vehicles, upper stages and associated debris in LEO-crossing orbits.

ISO 27852:2011 also clarifies the modelling approaches and resources for solar and geomagnetic activity modelling; the resources for atmosphere model selection; and an approach for satellite ballistic coefficient estimation.


General information

  • Status :  Withdrawn
    Publication date : 2011-07
  • Edition : 1
    Number of pages : 28
  • :
    ISO/TC 20/SC 14
    Space systems and operations
  • 49.140
    Space systems and operations

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