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About This Item

 

Full Description

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.

 

Document History

  1. ISO 23312:2022


    Space systems - Detailed space debris mitigation requirements for spacecraft

    • Most Recent
  2. ISO 26872:2019


    Space systems - Disposal of satellites operating at geosynchronous altitude

    • Historical Version
  3. ISO 16164:2015


    Space systems - Disposal of satellites operating in or crossing Low Earth Orbit

    • Historical Version
  4. ISO 16127:2014


    Space systems - Prevention of break-up of unmanned spacecraft

    • Historical Version
  5. ISO 23339:2010


    Space systems - Unmanned spacecraft - Estimating the mass of remaining usable propellant

    • Historical Version
  6. ISO 26872:2010

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    Space systems - Disposal of satellites operating at geosynchronous altitude

    • Historical Version