ISO 24352:2023

International Standard   Current Edition
· Approved on 04 May 2023 ·

Technical requirements for small unmanned aircraft electric energy systems

Aircraft and space vehicles in general
Including aircraft performance, flight dynamics, etc.

ISO 24352:2023 Files

English 19 Pages
Current Edition
153.28 USD

ISO 24352:2023 Scope

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.

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