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About This Item

 

Full Description

This document defines detailed space debris mitigation requirements and recommendations for the design and operation of unmanned spacecraft in Earth orbit.

This document defines detailed requirements that are applicable to:
a) avoiding the intentional release of space debris into Earth orbit during normal operations;
b) avoiding break-ups in Earth orbit;
c) disposal of a spacecraft after the end of mission;
d) estimating the mass of the remaining usable propellant;
e) developing and maintaining the space debris mitigation plan.

NOTE This document does not cover nuclear power sources on spacecraft.
 

Document History

  1. BS ISO 23312:2022

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    Space systems. Detailed space debris mitigation requirements for spacecraft

    • Most Recent
  2. BS ISO 26872:2019


    Space systems. Disposal of satellites operating at geosynchronous altitude

    • Historical Version
  3. BS ISO 16164:2015


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

    • Historical Version
  4. BS ISO 16127:2014


    Space systems. Prevention of break-up of unmanned spacecraft

    • Historical Version
  5. BS 12/30213836 DC


    BS ISO 16127. Space systems. Prevention of break-up of unmanned spacecraft

    • Historical Version
  6. BS ISO 23339:2010


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

    • Historical Version
  7. BS ISO 26872:2010


    Space systems. Disposal of satellites operating at geosynchronous altitude

    • Historical Version