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ISO 24352:2023

Current Revision

Technical requirements for small unmanned aircraft electric energy systems

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This document provides technical requirements and test methods for small unmanned aircraft electric energy systems (EESs).

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.


SDO ISO: International Organization for Standardization
Document Number ISO 24352
Publication Date Not Available
Language en - English
Page Count
Revision Level
Supercedes
Committee ISO/TC 20/SC 16
Publish Date Document Id Type View
Not Available ISO 24352:2023 Revision