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ISO 24352:2023

Technical requirements for small unmanned aircraft electric energy systems

Standard Details

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.

General Information

Status : Published
Standard Type: Main
Document No: ISO 24352:2023
Document Year: 2023
Pages: 19
Edition: 1
  • ICS:
  • 49.020 Aircraft and space vehicles in general

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ISO 24352:2023
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