ISO-24354 › General requirements for the payload interface of civil unmanned aircraft systems

ISO-24354 - 1ST EDITION - CURRENT


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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).

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49.020 (Aircraft and space vehicles in general Including aircraft performance, flight dynamics, etc. Air transport, see 03.220.50)

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Document Number

ISO 24354:2023

Revision Level

1ST EDITION

Status

Current

Publication Date

Aug. 1, 2023

Committee Number

ISO/TC 20/SC 16