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ISO 24354:2023

Current Revision

General requirements for the payload interface of civil unmanned aircraft systems

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This document specifies the composition, functional and performance requirements for a payload interface of civil unmanned aircraft systems (UAS), with the maximum take-off mass of 0,25 kg to 25 kg which relates to level II through IV according to ISO 21895.

This document is applicable to the design and manufacture of physically independent payload interfaces which connect an external payload to an unmanned aircraft (UA).


SDO ISO: International Organization for Standardization
Document Number ISO 24354
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 24354:2023 Revision