60.60 Standard published Aug 3, 2023
ISO
ISO/TC 20/SC 16 Unmanned aircraft systems
International Standard
49.020 Aircraft and space vehicles in general
Published
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).
PUBLISHED
ISO 24354:2023
60.60
Standard published
Aug 3, 2023