International Standard
ISO 16679:2015
Space systems — Relative motion analysis elements after LV/SC separation
Reference number
ISO 16679:2015
Edition 1
2015-09
International Standard
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ISO 16679:2015
57399
Published (Edition 1, 2015)

ISO 16679:2015

ISO 16679:2015
57399
Format
Language
CHF 63
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Abstract

ISO 16679:2015 provides relative motion analysis elements after LV/SC separation, including analysis input, analysis principle, analysis method and analysis output. It is applicable to the mission design and verification for the prediction of relative motion after LV/SC separation.

This International Standard focuses on the relative motion between the objects involved in one launch mission. It does not cover the issues about the collision avoidance between newly launched objects and on-orbit ones.

General information

  •  : Published
     : 2015-09
    : Close of review [90.60]
  •  : 1
     : 10
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

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