Informējam, ka Sistēma pielāgota darbam ar interneta pārlūkprogrammu Internet Explorer (8. un jaunākām versijām) un Mozilla Firefox (3.6 un jaunākām versijām).
Izmantojot citu interneta pārlūkprogrammu, brīdinām, ka Sistēmas funkcionalitāte var tikt traucēta.
<p class="MsoBodyText"><span lang="EN-GB">This document provides technical requirements and test methods for small unmanned aircraft electric energy systems (EESs).</span></p>
<p class="MsoBodyText"><span lang="EN-GB">This document applies to the EES of small unmanned aircrafts (UAs) with the maximum take-off mass (MTOM) less than 25 kg corresponding to unmanned aircraft systems (UASs) at level I, II, III and IV as graded in ISO 21895:2020, and with secondary lithium batteries. This document can apply to new type of batteries to be used in the UA electric energy system in the future.</span></p>
Reģistrācijas numurs (WIID)
78481
Darbības sfēra
<p class="MsoBodyText"><span lang="EN-GB">This document provides technical requirements and test methods for small unmanned aircraft electric energy systems (EESs).</span></p>
<p class="MsoBodyText"><span lang="EN-GB">This document applies to the EES of small unmanned aircrafts (UAs) with the maximum take-off mass (MTOM) less than 25 kg corresponding to unmanned aircraft systems (UASs) at level I, II, III and IV as graded in ISO 21895:2020, and with secondary lithium batteries. This document can apply to new type of batteries to be used in the UA electric energy system in the future.</span></p>
