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ISO 26872:2010

Withdrawn

Withdrawn

View Superseded by

Space systems — Disposal of satellites operating at geosynchronous altitude

Available format(s)

PDF

Language(s)

English

Published date

09-03-2010

Withdrawn date

04-09-2025

Superseded by

ISO 26872:2019

US$96.00
Excluding Tax where applicable

ISO 26872:2010 specifies requirements for the following:

  • planning for disposal of satellites operating at geosynchronous altitude to ensure that final disposal is sufficiently characterized and that adequate propellant will be reserved for the manoeuvre;
  • selecting final disposal orbits where the satellite will not re-enter the operational region within the next 100 years;
  • executing the disposal manoeuvre successfully;
  • depleting all energy sources on board the vehicle before the end of its life to minimize the possibility of an event that can produce debris.

ISO 26872:2010 provides techniques for planning and executing the disposal of space hardware that reflect current internationally accepted guidelines and consider current operational procedures and best practices.

Committee
ISO/TC 20/SC 14
DevelopmentNote
Supersedes ISO/DIS 26872. (09/2010)
DocumentType
Standard
Pages
53
PublisherName
International Organization for Standardization
Status
Withdrawn
SupersededBy

Standards Relationship
SAC GB/T 32308 : 2015 Identical
BS ISO 26872:2010 Identical

PD ISO/TR 18146:2015 Space systems. Space debris mitigation design and operation guidelines for spacecraft
BS ISO 16699:2015 Space systems. Disposal of orbital launch stages
ISO 16699:2015 Space systems — Disposal of orbital launch stages
ISO/TR 20590:2017 Space systems - Debris mitigation design and operation manual for launch vehicle orbital stages
BS ISO 23339:2010 Space systems. Unmanned spacecraft. Estimating the mass of remaining usable propellant
ISO 23339:2010 Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant
13/30235933 DC : 0 BS ISO 16699 - SPACE SYSTEMS - DISPOSAL OF ORBITAL LAUNCH STAGES
ISO/TR 18146:2015 Space systems — Space debris mitigation design and operation guidelines for spacecraft
PD ISO/TR 20590:2017 Space systems. Debris mitigation design and operation manual for launch vehicle orbital stages

ISO 16127:2014 Space systems — Prevention of break-up of unmanned spacecraft
ISO 24113:2011 Space systems — Space debris mitigation requirements

US$96.00
Excluding Tax where applicable