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ISO 26872:2010

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

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withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Space systems Disposal of satellites operating at geosynchronous altitude

Available format(s)

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

Withdrawn date

05-07-2019

Language(s)

English

Published date

03-09-2010

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.

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Withdrawn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

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

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