Space systems Relative motion analysis elements after LV/SC separation

Available format(s)

Hardcopy , PDF 1 User , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English

Published date

21-09-2015

Publisher

International Organization for Standardization

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.

DevelopmentNote	Supersedes ISO/DIS 16679. (09/2015)
DocumentType	Standard
Pages	10
PublisherName	International Organization for Standardization
Status	Current

Standards	Relationship
BS ISO 16679:2015	Identical

ISO 14303:2002	Space systems — Launch-vehicle-to-spacecraft interfaces
ISO 10784-1:2011	Space systems Early operations Part 1: Spacecraft initialization and commissioning
ISO 10784-3:2011	Space systems Early operations Part 3: Commissioning report
ISO 10784-2:2011	Space systems Early operations Part 2: Initialization plan