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ISO 27852:2016

Space systems — Estimation of orbit lifetime

Standard Details

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Status : WITHDRAWN
Standard Type: Main
Document No: ISO 27852:2016
Document Year: 2016
Pages: 43
Edition: 2
  • ICS:
  • 49.140 Space systems and operations

Life Cycle

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ISO 27852:2016
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