Standard

ISO 27852:2016

Withdrawn

Note: This standard has a new edition: ISO 27852:2024

Preview

Corrigenda and amendments are bought separately.

Language
Services

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.

Document information

  • Standard from ISO
  • Published:
  • Withdrawn:
  • Expires:
  • Edition: 2
  • Version: 1
  • Document type: IS
  • ICS 49.140
  • ISO TC ISO/TC 20/SC 14

Product Relations

Product life cycle