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About This Item

 

Full Description

ISO 23339:2010 gives requirements for estimating the mass of the remaining usable propellant of an unmanned spacecraft in low Earth orbit (LEO) or geostationary Earth orbit (GEO), and for designing propellant measurement systems. It is applicable to spacecraft with either mono- or bi-propellant propulsion systems using liquid or gaseous chemical propellants, and is limited to such systems because they are the most common for spacecraft in LEOs and GEOs.

 

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

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

    • Historical Version
  6. ISO 26872:2010


    Space systems - Disposal of satellites operating at geosynchronous altitude

    • Historical Version