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Product Product ISO 24352:2023
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Description Description

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.

Standard Number Standard Number ISO 24352:2023
Title Title ISO 24352:2023 Technical requirements for small unmanned aircraft electric energy systems
Status Status Published
Publication Date Publication Date 04 May 2023
Cross References Cross References
Descriptors Descriptors
ICS ICS 49.020
Committee Committee ISO/TC 20/SC 16 Unmanned aircraft systems
ISBN ISBN
Publisher Publisher PECB Store
Format Format PDF
Delivery Delivery NO
Pages Pages 19
File Size File Size KB