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<p>ISO 26872:2010 specifies requirements for the following:</p>
<ul>
<li> 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;</li>
<li> selecting final disposal orbits where the satellite will not re-enter the operational region within the next 100 years;</li>
<li> executing the disposal manoeuvre successfully;</li>
<li> 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.</li>
</ul>
<p>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.</p>
Reģistrācijas numurs (WIID)
43853
Darbības sfēra
<p>ISO 26872:2010 specifies requirements for the following:</p>
<ul>
<li> 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;</li>
<li> selecting final disposal orbits where the satellite will not re-enter the operational region within the next 100 years;</li>
<li> executing the disposal manoeuvre successfully;</li>
<li> 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.</li>
</ul>
<p>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.</p>
