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     : Withdrawn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
  • Technical Committee
     : ISO/TC 20/SC 14 Space systems and operations
  • ICS
     :
    49.140 Space systems and operations

Life cycle

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