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Withdrawn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Withdrawn (Edition 2, 2016)

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

  •  : Withdrawn
     : 2016-07
    : Withdrawal of International Standard [95.99]
  •  : 2
     : 43
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

Got a question?

Check out our Help and Support